[Military Pipe-Line Systems]
[From the U.S. Government Publishing Office, www.gpo.gov]

WAR DEPARTMENT TECHNICAL MANUAL J
NON-CIRCULATING
MILITARY
PIPE-LINE
SYSTEMS
- \
NTSU LIBRARY
Document Reserve

WI.35'./5'-3S'd>
fTAR DEPARTMENT • 15 NOVEMBER 1943
WAR DEPARTMENT TECHNICAL MANUAL
™5-350
MILITARY
PIPE-LINE
SYSTEMS
War Department • 15 November 1943
United States Government Printing Office Washington : 1943
This manual supersedes TM 5-350 (Tentative), 1 May 1943
WAR DEPARTMENT, Washington 25, D. C., 25 October 1943.
TM 5-350, Military Pipe-line Systems, is published for the information and guidance of all concerned.
[A. G. 300.7 (31 Aug 43).]
By order of the Secretary of War:
G. C. MARSHALL,
Chief of Staff.
Official:
J. A. ULIO,
Major General,
The Adjutant General.
Distribution:
B and H (3).
(For explanation of symbols see FM 21-6.)
MILITARY PIPE-LINE SYSTEMS • TM 5-350
CONTENTS
CHAPTER 1.	INTRODUCTION:
Paragraph
General i____________________________________ _	j
Uses for pipe-line system__________________________ 2
CHAPTER 2.	DESCRIPTION OF MILITARY PIPE-LINE EQUIPMENT:
Storage_____________________________________________________ 3
Pipe, couplings, and fittings, including repair accessories_	4
Pumping units_______________________________________________ 5
Control equipment___________________________________________ 5
Portable storage tanks______________________________________ 7
Communications______________________________________________ g
CHAPTER 3.	LAYOUT AND PLANNING:
Location of pipe line_____________________________________   9
Design of system. _________________________________________ 10
CHAPTER 4.	CONSTRUCTION:
Preparation of right-of-way________________________________ 11
Installation of communication system_______________________ 12
Primary distribution of pipe_______________________________ 13
Stringing pipe and couplings______________________________  14
Coupling the line__________________________________________ 15
Stream and river crossing__________________________________ 16
Installation of reciprocating pump station_________________ 17
Storage tanks______________________________________________ 18
Camouflage_________________________________________________ 19
CHAPTER 5.	OPERATION:
Testing of pipe line_______________________________________ 20
Starting the reciprocating pump____________________________ 21
Starting the pup centrifugal pump__________________________ 22
Starting the deep-well centrifugal pump_.___________________ 23
Intermittent pumping_______________________________________ 24
Restricted withdrawals_____________________________________ 25
Dispatching________________________________________________ 26
Gaging tanks_______________________________________________ 27
Maintenance and repair_____________________________________ 28
Communications_____________________________________________ 29
Safety precautions__________«.______________________________ 30
Phases of fuel supply______________________________________ 31
CHAPTER	6.	AUTOMATIC AND MANUAL CONTROL:	Paragraph
Automatic control for reciprocating pumps__________________ 32
Adjustment of control units________________________________ 33
Manual control_____________________________________________ 34
Troubleshooting__________________________________________   35
CHAPTER	7.	CENTRIFUGAL PUMP OPERATIONS:
General____________________________________________________ 36
Pup centrifugal pump_______________________________________ 37
Pump station operation with 4-inch pipe line_______________ 38
Pump station operation with 6-iilch pipe line______________ 39
Control of pup centrifugal pump on two-pump station installation_______________________________________________________ 40
Trouble shooting___________________________________________ 41
Deep-well centrifugal pump_________________________________ 42
CHAPTER 8.	PIPE-LINE PERSONNEL AND ORGANIZATION:
Commissioned officer personnel for construction and operation. 43
Enlisted personnel for construction and operation__________ 44
CHAPTER 9.	PETROLEUM PRODUCTS TESTING LABORATORY:
General____________________________________________________ 45
Tests which can be made with petroleum products testing laboratory sets____________________________________________ 46
Base laboratory____________________________________________ 47
Portable laboratory_______________________________________  48
Petroleum products testing laboratory apparatus, equipment, and supplies_______________________________________________ 49
APPENDIX I. SPECIFICATIONS:	Pa6e
Military 4-inch pipe-line section________________________ 157
Military 4-inch pipe-line valve sections_________________ 159
Military pipe-line pumping station_______________________ 160
Military 4-inch pressure-reduction station_______________ 163
Military 6-inch pipe-line section________________________ 164
Military 6-inch pipe-line valve sections_________________ 165
Military 6-inch pressure-reduction station_______________ 166
Manifold, two-unit, for 6-inch military pipe line________ 167
Pump, centrifugal, two-stage, series-parallel operation, gasolineengine driven____________________________________________ 170
Tanks: steel, gasoline, vertical,	bolted_________________ 171
APPENDIX II.	SELECTED REFERENCES_______________________________________ 177
This manual supersedes TM 5-350 (Tentative), 1 May 1943.
CHAPTER 1
INTRODUCTION
1. GENERAL. This manual describes equipment, layout and planning, construction, operation, maintenance, and operating personnel organization for the portable pipe-line system designed for military use. Transmission capacities, using lightweight 4- and 6-inch pipe, are 200 and 400 barrels per hour, respectively. Associated pumping and control equipment has been designed for these capacities and for operation at 200 pounds per square inch.
2. USES FOR PIPE-LINE SYSTEM, a. Pipe line systems were designed to provide a means for transmitting, distributing, and storing bulk liquids in theaters of operations, and pipe-line equipment is considered to embrace all that is necessary for carrying out such operations.
b.	Pipe lines will ordinarily be used to make bulk deliveries of gasoline or water from terminals
to distribution points. More specifically, they can be used for—
(1)	Transmission of liquids over terrain too rugged for other means of transportation.
(2)	Relief of congestion where road capacity is limited and traffic is heavy.
(3)	Rapid transmission of liquids over long distances.
(4)	Transmission of liquids over short distances where conditions arising from enemy action make other means of transportation impracticable.
c.	Military pipe lines may also be used to ship crude petroleum from producing fields to shipping terminals or refineries.
d.	Tests to determine a procedure for constructing and laying ship-to-shore submarine pipe lines are planned. Upon completion of such tests a supplementary manual outlining a recommended procedure will be issued.
1
CHAPTER 2
DESCRIPTION OF MILITARY PIPE-LINE EQUIPMENT
3.	STORAGE.
a.	Storage Tanks. Storage at terminals or loading locations normally will be in bolted steel tanks, with capacities ranging from 100 to 10,000 barrels (42 U. S. gallons equal 1 barrel). These tanks are to be supplied in accordance with American Petroleum Institute specifications, as modified for military use. (See app. I.) Bolted tanks will be shipped “knocked down” with bolts, gaskets, and fittings for erection. Pressure and vacuum release values are supplied with all sizes of tanks.
b.	Storage Barges. For temporary or semipermanent storage at the source, there are several types of standard approved Army and Navy tank barges. These barges range in size from small ones of 21-foot beam and 43-foot length, 4-foot draft and capacity of 350 barrels, to large self-propelled barges of 43-foot beam and 107-foot length, 4-foot draft and capacity of 1,750 barrels. Discharge equipment is not a part of the barge and must be furnished as extra equipment.
c.	Collapsible Containers. Collapsible containers have been developed for the storage of petroleum products, including high octane or aromatic gasoline. These cells or bags are constructed of synthetic rubber impregnated fabric, supported in suitable containers of duck or plywood panels.
(1	) The cells are made for both stationary and portable service, in capacities ranging from 7% to 3,000 gallons, and are designed for use where transportation space and time of erection are controlling factors. Figures 1 and 2 show a 3,000-gallon cell of the type used for stationary storage; figures 3 and 4 show a 2,700-gallon cell of the type used for bulk transportation by rail. There is a 750-gallon tank, similar to that shown in figure 4, which is used for bulk transportation by truck (2%-ton 6 by 6, cargo).
(2	) Three men can assemble a 3,000-gallon tank in 30 minutes, but a 2,700-gallon tank for stationary storage requires about 4 hours.
(3	) Complete assembly instruction is furnished with each cell. In handling collapsible containers, care must be exercised that the treated fabric is not damaged by dragging it along the ground, walking upon it, or refolding it about tools and fastenings.
4.	PIPE, COUPLINGS, AND FITTINGS, INCLUDING REPAIR ACCESSORIES.
a.	Pipe. Lightweight pipe of the spiral or longitudinal weld types is commonly used. The 4- and 6-inch standard sizes of pipe are made of 14-and 12-gage steel, respectively. (See app. I.) For heavy wall pipe, standard American Petroleum Institute specifications have been adopted for both 4- and 6-inch sizes. All pipe is grooved on each end to accommodate Victaulic type couplings, and is supplied in standard lengths of 20 feet. The lightweight pipe is reinforced at the grooved ends.
b.	Couplings. Victaulic type flexible pipe couplings (fig. 5) are utilized for military pipe lines. They allow for some degree of anguTar deflection and contraction or expansion. Such couplings are composed of a malleable iron housing in two or more parts (held together by two or more track neck bolts), which mechanically engage and lock adjacent grooved or shouldered pipe ends in a positive couple. A single, continuous, hollow-moulded, composition, sealing gasket, C-shaped in cross-section, is so installed that internal pressure or vacuum serves to increase the tightness of the seal. All of the standard types of fittings, such as elbows, reducers, tees, and crosses, may be obtained at equipment pools, with grooves for use with Victaulic type couplings.
c.	Gate Valves. Commercial type gate valves of either flange, screw, or weld design are available, installed in joints of pipe fabricated to 20-foot total over-all length (fig. 6). (See app. I.)
d.	Check Valves. Commercial type check valves are installed in joints fabricated into 20-foot lengths for installation at any point in
2
Figure 1. Stationary collapsible container, partially assembled.
Figure 2. Stationary collapsible container, capacity 3,000 gallons.
3
Figure 3. Transport collapsible container, partially assembled.

Figure 4. Transport collapsible container, capacity 2,700 gallons.
4
i Firm	rmn
OPERATING FEATURES	____S...1’. L_ _ !?_ & /
________ i—i —n E 6 rt
WMBBV	WBI BRB	__1 
()	9 4* PIPE	6" P/PE
L_
INSTALLED	PRESSURE SEAL
--------------------- \	/		 .«	4" pipe = sj’_	/a MOULDED GASKET SHAPE-\	/	SUCTION SEAL_E^P! PE	* ■■'
K /'' LI Ar \ A
IB la 13. I* IB Mt 'Hh’ * v yF O <	BBesEB __	['pp	~ /’j" i h^h^B’
MfW’	IT__L \
-------- —1----------------	L—	^krw - - --■
VALVE PIPE SECTION
— FW 10 — FW 13 ^FW 11 — FW 8 — FW 9 —FW 6 -FW 5 — FW 19 — FW 7 -"FW 12 ^FW 2
"FW 3 — FW 4 ^FW 18
— FW 14
— FW 17 — FW 16
— FW 15
— FW 1
PART FW	1	BODY
PART FW	2	BONNET
PART FW	3	BONNET STUD
PART FW	4	BONNET STUD NUT
PART FW	5	STUFFING BOX
PART FW	6	GLAND
PART FW	7	STUFFING BOX PACKING
PART FW	8	STUFFING BOX & GLAND STUD
PART FW	9	STUFFING BOX & GLAND STUD NUT
PART FW	10	LOCKING PIN
PART FW	11	HAND WHEEL
PART FW	12	STEM
PART FW	13	STEM NUT
PART FW	14	NUT WEDGE
PART FW	15	LOOSE WEDGE
PART FW	16	DISC
PART FW	17	SEAT
PART FW	18	BONNET GASKET
PART FW	19	STUFFING BOX GASKET
Figure 6. Gate valve.
CHECK & GATE VALVE PIPE SECTION
V--------- 4" WHEATLEY TWIN GATE & CHECK VALVE
--------GROOVE FOR COUPLING	\
*	X	A———------------------------------------A	X
HW-3925	"' A"GATE VALVE	HW-3925
4 "standard pipe
STANDARD 20'SECTION
Figure 7. Check and gate valve pipe section.
FWT 25
FWT 27
FWT 18
FWT 24
FWT 23
FWT 19
FWT 22
FWT 20
FWT 21
-FWT 10 ' FWT 13 FWT 11			
“FWT	8	PART	FWT 1
“FWT	9	PART	FWT 2
“FWT	6	PART	FWT 3
-FWT	5	PART	FWT 4
FWT 28 -FWT 7 -FWT 12		PART PART PART PART PART PART	FWT 5 FWT 6 FWT 7 FWT 8 FWT 9 FWT 10
‘FWT	2	PART	FWT 11
FWT	3	PART	FWT 12
SFWT	4	PART	FWT 13
FWT	26	PART	FWT 14
FWT	17	PART PART PART PART PART PART PART	FWT 15 FWT 16 FWT 17 FWT 18 FWT 19 FWT 20 FWT 21
FWT	14	PART	FWT 22
FWT	16	PART	FWT 23
FWT FWT	15 1	PART PART PART PART	FWT 24 FWT 25 FWT 26 FWT 27
PART FWT 28
BODY
BONNET
BONNET STUD
BONNET STUD NUT STUFFING BOX GLAND
STUFFING BOX PACKING
STUFFING BOX, GLAND STUD STUFFING BOX, GLAND NUT LOCKING PIN HAND WHEEL STEM STEM NUT NUT WEDGE LOOSE WEDGE DISC SEAT CHECK COVER CHECK DISC CHECK DISC NUT COTTER PIN CHECK ARM HINGE PIN PIN HOLE PLUG CHECK SEAT BONNET GASKET CHECK COVER GASKET STUFFING BOX GASKET
8
DOUBLE GATE AND REVERSIBLE CHECK VALVE
SYNTHETIC SEAL ON CHECK IS OPTIONAL
9
SYNTHETIC RUBBERrA SEAL	f
—d
----LENGTH OF VALVE 2.-4^" --------------- ----OVERALL LENGTH OF VALVE
AND PIPE 3O£"
Figure 8. Double gate and reversible check valve.
4" PRESSURE REDUCING STATION
/--HANLON-WATERS TYPE 1628-4'
-GROOVE FOR COUPLING /\
^HW-3924	4"GATE VALVES	HW-3924
'^~Z-----------------------------------------------------------------------
REGULATOR SECTION
■*------------------------------STANDARD 20' SECTION----------------------------
PARTS LIST
HW-107 SPRING CAP HW-139-A BODY GASKETS HW-142-B SPRING
HW-1909 SPRING
HW-2037 VALVE STEM BUSHING
HW-2765 ADJUSTING SCREW
HW-2820 UPPER SEAT RING
HW-2821 LOWER SEAT RING
HW-2899 SPRING SEAT
HW-3776 UPPER DISC
HW-3778 LOWER DISC
HW-3905 DIAPHRAGM PLATE
HW-3908 UPPER BACK-UP PLATE
HW-3909 UPPER PLUG GUIDE
HW-3910 LOWER PLUG GUIDE
HW-3911 DIAPHRAGM
HW-3933 VALVE STEM
A-791 BOTTOM PLATE
A-792 LOWER DIAPHRAGM CASING
A-793 UPPER DIAPHRAGM & SPRING CASE
A-797 VALVE BODY
HW-107 HW-2765 HW-2899 HW-1909 |'-13THD HEX NUTS HW-3905 HW-3911 |"x2|CAP SCREW W/NUT
PRESSURE GAUGE
4 ELBOW
HW-2821
HW-3909
-----n~w
A-791
4x6 NIPPLE A-792 —
HW-2037
HW-3933
A-797—
SET SCREW HW-142-B A-793
q" o'/
x if CAP SCREW
1"- 13 THD.HEX. NUT HW-139-A
HW-3910
HW-3778
13 THD.HEX. NUT
HW-2820
HW-3776
HW-3908
HW-139-A |x 1|"CAP SCREW
Figure 9. Regulator and regulator section Jor downhill installations.
10
Figure 10. Split repair clamp made up of two half-shells.
figure 11. Half-shell of split repair clamp used with stirrup bolts.
11
CORPS OF ENGINEERS
Figure 12. Saddle repair clamp.
figure 13. Dresser type split clamp for use over Fictaulic type couplings.
12
PLAN VIEW OF STATION ARRANGEMENT...SMALL PUMPING UNIT
belt guard
HW-3791
mA - 3920
■' HW-3797-'
Sample to be taken here
UP-STREAM±
FLOW
DOWN-STREAM
■4jheck VALVE
HW - 3793
SECTION
NO. 1
SUCTION
HEADER
SECTION
NO. 5 ( intone)
SECTION
NO.3 (intone)
DISCHARGE
HEADER
MAIN LINE HEADER SECTION
SUCTION VALVE
?IG. <860 - 4 j sjASQ.p> IMP
DISCHARGE VALVE
HIGH SUCTION RELIEF - HANLOM" WATERS TYPE 1627-A
SAND TRAP SECTION NO. 2
BUU~ LWmE
MuDH H 4 TH
CONTROL panel
HW-392C 1
HAN LON-WATERS TYPE ’626-A
HIGH DISCHARGE RELIEF,
NDUlT PIPE
-A 737
SAND TRAP
hw-3731
DISCHARGE LINE
Battery box
ENGINE GOVERNOR OIL RESERVOIR
Figure 14. Plan view of small reciprocating pump station arrangement.
552517 0 - 43 -2
13
NO V.i.-tiC 2 i‘BURGESS -
ExhauS1" SNUBBER
PLAN VIEW OF STATION ARRANGEMENT.. LARGE PUMPING UNIT
conw paw
—
battery box
-TOOL-BOX
___GASO PUMP FIG 1560
HW-3920
HW-3797
HW-3731
SAND TRAP
> Sample Iq be taken
here
DISCHARGE LINE i

FLOW

_ Figure 15. Plan view oj large reciprocating pump station arrangement.
MAIN LINE HEADER SECTION
SUCTION VALVE
MODEL MU-VO'-3 MAX V SILENCER
SECTION NO. 6
SAND TRAP SECTION NO. 2
ENGINE GOVERNOR
OH RESERVOIR
DISCHARGE HEADER
HANLON-WATERS
TYPE 1626-A
BUDA ENGINE
MODFt Jl-A
DISCHARGER
VALVE %
SECTION
NO. 5 (intone)
SECTION
NO.3 (in tone)
SECTION NO. 1 (intone)
_ ,..z U--..
UP-STREAM
.ZZ030
DOWN-STREAM
CHECK VALVE
SUCTION
HEADER
HIGH SUCTION RELIEF-HANLON “
WATERS TYPE 1627-A
14
y____	‘ • j
^HiGH DISCHARGE RELIEF^
WIRING DIAGRAM SYNCHRO-START IGNITION INTERRUPTER
GROUNDED TO FRAME
Figure 16. Wiring diagram, synchro-start ignition interrupter.
15
GROUNDED I TO FRAME
MAGNETO
RELAX	BOX
TO HOT SIDE OF AMMETER
\ PANEL
' SWITCH
centrifugal pump connected to a gear speed increaser built integrally with the pump (figs. 21 and 22). Connection to the engine is by means of a flexible coupling. The pump has two suction nozzles beneath and two discharge nozzles above, of the 4-inch Victaulic type, all of which are on the same side of the pump. Connecting pipe is supplied so that the two stages may be run either in series or in parallel (figs. 23 and 24). All pump parts are designed for a maximum working pressure of 700 pounds per square inch so that two units can be safely run in series. When the two impellers of one unit are operated in series at an engine speed of 1,950 revolutions per minute, the pump has a capacity of 200 barrels per hour at a differential pressure of 200 pounds per square inch when pumping 0.68 specific gravity gasoline.
(a) The pup unit is powered by a 6-cylinder General Motors model 270, 4-inch stroke, 269.5 cubic inches displacement, spark-ignition, water-cooled, automotive, gasoline engine. It is equipped with tachometer, overspeed governor, suction and discharge pressure gages, oil pressure shut-off switch, and water temperature safety shut-off switch.
(Z>) This unit is mounted on a skid fabricated from 8-inch H-beams and channels which are sufficiently strong to permit lifting on or off a truck. The total weight of the complete unit is about 2,000 pounds. (See app. I.)
(c) For a further description of this unit, see Manufacturers Parts List and Instruction Manuals furnished with each unit.
(2) The deep well unit consists of a vertical, six-stage, centrifugal pump with a V-belt drive. This pump has a capacity of 150 gallons per minute at 150-foot head (fig. 25). The pump is powered by a Wisconsin model AHH, sparkignition, air-cooled, industrial, gasoline engine (figs. 26 and 27). Engine and pump are mounted on a fabricated skid base. For further description of this unit see Manufacturers Parts List and Industrial Manuals, furnished with each pump.
c. Tools. All pumping units are equipped with a tool box containing tools and spare parts necessary for the maintenance and operation of the pumps and engines.
6.	CONTROL EQUIPMENT. This equipment may be either automatic or manual.
a.	Control Equipment for Reciprocating pumps.
(1)	Automatic control equipment supplied is
manufactured by Hanlon-Waters, Inc., and is the conventional diaphragm-actuated, spring-loaded type used in conjunction with hydraulic engine speed governors. This control equipment is mounted on the engine-control panel and is an integral part of the pumping unit. It is capable of performing the following functions automatically:
(a)	Control pumping rate so that the liquid received is pumped at a rate to maintain a predetermined suction pressure.
(6)	Control pressure differential between the suction and discharge at a predetermined limit, and distribute any additional load between that station and other stations on the suction side.
(c)	Control maximum discharge pressure of the pump at 650 pounds per square inch so that the pump will be automatically bypassed when a valve is closed on the discharge side of the pump.
(d)	Control engine throttle so that when the suction pressure exceeds a predetermined maximum pressure the engine speed will be reduced to idling.
(2)	Manual controls. Control equipment for manually controlled stations consists of pressure gages, gate valves, and engine throttle. A spring-loaded, high-pressure, bypass, relief valve is provided as a safety device.
b.	Control Equipment for Centrifugal Pump. Automatic safety shut-down controls to protect centrifugal pumps from excessive discharge pressure, high temperature, and abnormally low suction pressure will be provided on military pipe lines.
7.	PORTABLE STORAGE TANKS. Depending on the type of liquid to be handled, various types of portable tanks are available as follows:
a.	Steel tanks for gasoline and other petroleum fuels. (See app. I.)
b.	Adaptation of the collapsible container for gasoline and other petroleum fuels.
c.	Canvas tanks can be used for water storage.
8.	COMMUNICATIONS. U. S. Signal Corps field telephone equipment is standard for service with military pipe lines. Field radio and messengers may be also used. Field Manuals should be consulted for details on operation, installation, and maintenance of these types of communication systems.
16
PRESSURE SHUT-DOWN SWITCH FOR PUP PUMP
MANUAL RESET FRONT VIEW WITHOUT COVER	REAR VIEW
Figure 17. Pressure shut-down switch for Pup Pump.
17
n o. so hc z'/i burgess
/EX HAUS T snubber	MM bI I.V.t J J LI E (BilJ M Bl PJFkVM1J f tf W
GOVERNOR /	^^■U|iA13KCUZA|kMSAjXMA41hA^fl
/OIL RESERVOIR /	i"	■	.	.
/	/	conduit pipe	mMMWMWfv'wwiwWMWWWW
~~I—--------' rZN / : / W MHIMiKKliM
Pr/HT—ift U
V- Q 1	/ TOOL BOX [ ] I
&	/ w!
1 > n -Mn^r J—rW°	Sz^nnk -
=a.™ R / *T_JJ^^- RM ‘ R I box V< jrgyr'^ TXT T 5
__:____:____r---	- R~Ji—Mj---jRxg-j_ 1 "' ।_____
\3B PITCH DIAX5NQ 144-CX 28.8" PITCH DIA. SHEAVE
SHEAVE O.QHUB V-BELTS	SOLID OFFSET HUB
-T----------li'“E
_________Xgy	Rig- i860-4j"i6"
XF-—CS——GASO PUMFJ-
MODEL K-428
BUDA ENGINE	___	/4" DISCH. FLANGE 10" O.D.	._
fl I . । /8" i"studs 0N 7k bc	A wntrol panQx
ii''NLn Ml/	h®0®r
"®	sGES-t fifML=
..	x II — - --1 AP P—«	Is3JX-g/l •=!
Am	;; -m/ r Jk--.-	I mrr
• — *—■* -rr	' s\ || / ' —1 yp ~4~'\ 1 li^	। \°* • ° • *7 n II II
—I—1|	II I W.M~- ,	J,
«o|_-OR	«
II	A - p 'A	—a
4" FLANGE - 10" 0D.
8- I "HOLES ON 7-j’B.C.
Figure 18. Dimension drawing of small reciprocating pump unit.
18
Figure 19. View of small reciprocating pump unit.
19
___J	« MAXIM SILENCER
*	tz=J /MODEL MU-NO. 7-3j"	I—GAS0 PUMP FIG. 1560
‘<£	r	BATTERY	/
£	(J	80x	_ TOOL BOX I
-----------	JI	/	” I	~ 1 in nl J	~^E«Bt3’F •• =
----------t=ie=3b;:f^
- „n u	___________)
8-| STUD BOLTS ON 6" “I	/
/----DIA. BOLT CIRCLE IN	v~ SERIES CONNECTION
/ EACH FLANGE	\*F0R MAiN PIPE	)
L „	\ LINE USE)
If ■*-/ 8"—►!	DISCHARGE	DISCHARGE \	\
]-[&-----T<(VICTAULIC GROOVE)	V	/
//* —^^^VT-l-EZ------Loo SUCTION	|	\
\( ["TTfcJ !/(VICTAULIC GROOVE) ~L___________________________________________\ /
vx ■^2S!/2''LG.	18-8	2
98-1	LOCK SCREW - deflector - %"x72''LG.	STEEL	~T~
103 BLIND END BEARING_______ BEARIUM BRONZE 1
111 SPLIT GLAND_____________ HARD BRONZE	~
146 PIN - centersleeve - 3/g"x 334"LG. S.A.E. 10 20	~ 1
159	PUMP SHAFT_______________11.5-13%	CHR.ST'L.	1
161	DRIVESHAFT_______________S.A.E.	2340 H.T.	1
176'1	IMPELLER-1ST	STAGE_______HARD	BRONZE	1
176-2 IMPELLER-2ND STAGE_________” v 1
207 CASE WEAR RING______________BRONZE______2
229	CENTER BUSHING___________BEARIUM	BRONZE	1
236	CAGE RING	IHARD BRONZE	F
241 DEFLECTOR	BRONZE	~F
249 LOCKNUT ________________ MRC-N-Q6	F
257 LOCATING RING______________S.A.E. 10-20	1
257-1 LOCATING RING_______________»	»_____1
281	GEAR BOX COVER_______________C.	I._____1
281-1	BEARING HOLDER______________C.	I._____1
344	BALL BEARING SLEEVE________S.A.E.	1020	1
462	CONNECTOR__________________TdooT^s^	1
571	GEAR-DRIVEN__________caseA'hardened___1
572 GEAR-DRIVER_________________»	«______1
654	BALL BEARING_____________M R C <7407	1
654-1	BALLBEARING__________M R C * 7406
655	BALL BEARING______________ MRC*407R	2
673	LOCK WASHER_________________MRC-W-Q6	1
676-1 KEY-IMPELLER	11.5-13% CHR.ST’L. 2
676'2 KEY-GEAR-DRIVEN________n »>	>. „ ~F
676-3 KEY-GEAR-DRIVER__________S.A.E. 2340 H.T. 1
677 KEY-COUPLING__________________STEEL_____1_
686 NATIONAL Oil ^FAI	No. 50049 FOR 1’/♦"SHAFT i
OOP INAIIUNAL UIL otAL______ 200 FT/MIN. RUBBING SPEED 1
686*1 NATIONAL OIL SEAL	No.50055 FOR 1H"SHAFT	n
oou I INAIIUINAL	OCAL________200 FT/MIN. RUBBING SPEED 2
697 SPECIAL LOCK PLUG ~ center sleeve S.A.E. 10-20	1
742 PACKING RING	JOHN CRANE	6
756 GEAR BOX	| C. I, |~T~
PETTI HHHHMWWVPVmHMHI	I3WQ
24
@@)@@@)@(^@
DEEP WELL PUMPING UNIT
SECTION & DIMENSION DRAWING FOR 6 STAGE - MODEL NO. PI - 606
—"1 1 ■<"csg5ais>
rfw •	I	SS^ST \ \ x
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L ip~ri — - ■ -1- 1	~	\ F*------	■-----z ||	•****
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Figure 25. Section and dimension drawing of deep-well pump unit..
25
AIR CLEANER
BREATHER
LINE '
CARBURETOR
CHOKE LEVER
-OPEN- K
CARBURETOR*
NEEDLE VALVE
magneto
SWITCH *
WISCONSIN ENGINE
FOR DEEP WELL UNIT
GOVERNOR
CONTROL
Fi-YWHEEL
Magneto
BREAKER COVER
STARTING SHEAVE
Figure 26. Front view oj Wisconsin engine J or deep-well unit.
26
CHAPTER 3
LAYOUT AND PLANNING
9.	LOCATION OF PIPE LINE.
a.	Reconnaissance.
(1)	After study of existing maps the first step in determining the location of a pipe line is to make a ground reconnaissance of the country through which the line is to be laid. Knowledge of the topography thus gained will enable the engineer to choose the most suitable route for the line, both from the standpoint of military necessity and from that of good pipe-line practice. The most nearly level route should be chosen whenever possible. Natural cover, such as brush and trees, should be used in order to protect the line from enemy observation. A route along the bank of a stream is seldom desirable, especially where the stream is likely to overflow its banks.
(2)	Wherever possible the pipe line should be located more or less parallel to an existing road or trail, in order to facilitate the transportation of pipe and requisite equipment along the route of the pipe line. Speed of construction will in a large measure depend upon the prompt supply of component parts of the pipe-line system along the site. (3) If contour maps of the area are available, they can be used to great advantage in supplementing reconnaissance information. Airplane flights and aerial maps are also valuable aids in choosing the best route for a pipe line, particularly from the standpoint of locating the line so as to conceal it from enemy aerial observation.
b.	Survey.
(1)	When the approximate route for the pipe line has been chosen, a survey must be made to determine its bearing, length, and elevation changes (profile). There are several methods of surveying the route which are practicable and sufficiently accurate for designing a workable pipe-line system. Each of these methods will be outlined in some detail. As the survey progresses the course of the pipe line should be marked for the benefit of the construction and installation crews. Wooden
stakes, placed at approximately 500-foot intervals in wooden areas and at approximately greater intervals in open areas, are used for this marking. In wooded and brushy areas the route can be plainly marked by tying small strips of cloth or drafting tape to trees and brush along the line between stakes. Notes should be made of the location of all clearings and wooded areas, stream and river crossings, road crossings, and other points of possible future interest.
(2)	When the pipe-line system has been designed and the location of pump stations, block and check valves, and pressure-reducing regulators determined, their location along the line should be plainly marked with stakes. Following is a list of stake colors which may be used for this marking:
Location	Stake color	Remarks
Route	 Pump station	 Gate block valve	 Check valve	 Reducing regulator. Loading station	 Branch line		Plain	 Blue. ...	Number stakes in sequence. Mark pump station number on stake as well as distance from Station No. 1.
	Green	 Yellow	 Red		
	Orange	 White		Place 2 stakes, 1 on main route and 1 about 20 feet toward branch line.
(3)	Use of contour maps. The course of the line is plotted on contour maps of the area to be traversed (fig. 28). Starting at the source (Station No. 1), a profile of the pipe-line route is plotted showing ground elevation at all critical points, such as ridges, valleys, and abrupt changes in slope, over the entire length of the line (fig. 29). This profile should be plotted with a vertical scale of 1 inch equals 500 feet and a horizontal scale of 1 inch equals 5 miles. If more detail of the route
27
between some of the stations is desired, the profile may be plotted with a vertical scale of 1 inch equals 500 feet, and a horizontal scale of 1 inch equals 2% miles. When the course of the pipe line has been first laid out on a contour map, it will be necessary to transfer it from the map to the ground. This should be done using stakes as previously outlined. In addition, several significant elevation changes should be checked with a transit, level, or barometer, to be sure that the profile constructed from the contour map is an accurate representation of the ground.
(4)	Use of aneroid barometer and compass.
(a)	If no contour map is available, a simple, rapid survey can be made using an aneroid barometer and compass. Accompanying distances are obtained from a map or by chain, tape, foot pace, or automobile speedometer.
(6)	When an aneroid barometer is used, elevation at all critical points along the proposed route should be recorded. Careful use of the barometer will insure the measurement of approximate elevations. At the time elevations are measured the location and length of the line are also obtained by compass survey. Data obtained by the compass survey consist of magnetic bearing and length of each segment of the line between the source and discharge. The length of each segment can be measured by chain, tape, or foot pacing. Where maps are available, or where the approximate route can be traversed by automobile, over-all distance thus obtained should be used, proportionate corrections being made in the individual segment lengths. A ground profile can be readily constructed from the elevation and distance measurements obtained.
(5)	Use of level and chain or transit and stadia. Surveys by level and chain, or by transit and stadia are the most accurate, but they consume considerable time and are applicable only to areas which are relatively inactive.
(6)	If reconnaissance of the proposed pipe-line route shows that the terrain to be crossed is fairly level and that the relief is compensating, a detailed elevation survey will not be necessary. The pipe line in this case can be laid in a straight line. Locations of the pump stations will depend on line friction, static head, and the suction pressure required at each station along the line, as will be discussed later in this manual.
10.	DESIGN OF SYSTEM. Inasmuch as military pipe lines are to be constructed with standard sizes of pipe and pumping equipment, the problem
28
of design need be based on the following considerations only: size of pipe available (4-inch or 6-inch), size of pumps available, and amount and kind of liquid to be delivered through the line. With these considerations established and with the ground profile plotted to a vertical scale of 1 inch equals 500 feet, and to a horizontal scale of 1 inch equals 5 miles, the next step is to compute the hydraulics of the system, in order to determine the number and location of pump stations and pressure reduction stations.
a. Modular System of Pipe-line Design. A detailed analysis of the hydraulics of a pipeline system is complicated; therefore a simplified method of pipe-line design, called the modular system, has been adopted, so named because it is a model measuring method of determining the location of pumping and pressure-reducing stations by combining static and friction heads on a hydraulic gradient triangle, the scales of which correspond to scales selected for the profile of the pipe-line route. This graphical method should be used by the survey engineer in the field during the progress of the survey.
(1)	The procedure to be followed in using the modular system for pipe-line design is as follows:
(a)	Knowing the kind of liquid and the rate at which it is desired to pump it, the friction pressure loss per mile is determined from figure 30 for 4-inch pipe, or from figure 31 for 6-inch pipe. For example, from figure 30 the friction loss for 4-inch spiral weld pipe carrying 200 barrels per hour of 0.70 specific gravity gasoline is 20 pounds per square inch per mile.
(b)	Having determined the friction loss per mile, a right triangle called a hydraulic gradient triangle is next made from a piece of heavy bristol board or other suitable material about 10 inches square. This triangle is constructed in the following described manner. Figure 32 also outlines the procedure for construction. The finished triangle is shown on figure 33.
1.	On the side of the piece of chosen material lay out a scale on its base or horizontal side using the same scale in miles per inch as was used on the profile. Make this scale cover a distance of at least 40 scale miles. Calibrate the scale in 1-mile divisions, or less if desired, although this is not essential. Make the zero point at the right angle of the triangle.
2.	Lay out the vertical side of the triangle to represent 2,500 feet on the same vertical scale used in plotting the profile. For example, if the vertical scale is 1 inch equals 500 feet, the
FUEL TANK AIR VENT
HOLE
WISCONSIN ENGINE
FOR DEEP WELLUNIT
SPARK PLUG
SPARK PLUG WIRE
GASOLINE
FLYWHEEL
GOVERNOR SPRING
GOVERNOR
CONTROL ROD
OIL DRAIN
Figure 27. Front view of Wisconsin engine for deep-well unit.
FUEL
strainer
OIL FILLER PLUG
THROTTLE LEVER
FUEL
LINE
GOV.
LEVER
552517 0 - 43 -3
29
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Figure 29. Profile of pipe-line route.
DISTANCE - MILES
Figure 28. Route of pipe line on contour map.
30
PIPE LINE ON CONTOUR MAP thfater of operations ■ STATION ? REDUCING REGULATOR SCALE -1	10 MILES
RATE BARRELS PER HOUR
PRESSURE DROP-POUNDS PER SQUARE INCH PER MILE
Figure 30. Flow of gasoline and water in 4-inch pipe.
31
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side of the triangle will be 5 inches long. Graduate this vertical side in hundreds of feet with the zero point at the top of the triangle. This scale in feet represents the static head in feet of the flowing liquid Convert this head in feet to static head in pounds per square inch by using the following equation:
P HXS 2.31
where P=pressure in pounds per square inch, H = head in feet of flowing liquid, and
S = specific gravity of flowing liquid.
Using the above relation, compute the number of feet of head corresponding to 50 pounds per square inch static head. In the case of gasoline with a specific gravity of 0.70, this value will be 165 feet. Subdivide the vertical scale on the side of the triangle into units of 165 feet each, beginning at the zero end of the scale, each unit representing 50 pounds per square inch static head. In the example, these units will be plotted at 165 feet, 330 feet, 495 feet, etc., the 2,500 foot static head being equal to 758 pounds per square inch.
3.	The friction loss in pounds per square inch per mile obtained above is used to establish the slope of the hypotenuse of the hydraulic gradient triangle by dividing the total length of the vertical scale in terms of pounds per square inch static head by the friction loss in pounds per square inch per mile. For example:
™ = 37 9 20
This factor of 37.9 denotes the point on the base, or horizontal side on the scale of miles used, from which a connecting line is drawn to the zero point on the vertical side of the triangle, thus delineating the hypotenuse. Complete the triangle by cutting along the hypotenuse. It should be noted that the slope of this hypotenuse represents the friction loss in pounds per square inch per mile for a particular size of pipe carrying a particular liquid at a predetermined rate. A change in either the size of pipe, the type of liquid, or the rate of flow requires the construction of another hydraulic gradient triangle.
b. Example. Determine the location of and the number of pumping stations required on the pipe line shown in plan on figure 28 and in profile on figure 29.
(1)	Conditions:
Throughput_______ 200 barrels per hour.
Pump pressure. _ 30 pounds per square inch suction, 230 pounds per square inch discharge.
Pipe line________4 inch spiral weld.
Liquid___________0.70 specific gravity	gasoline.
Pump unit________ small reciprocating.
(2)	Several general statements regarding pipe-line design and operation should be noted before proceeding with the task of locating pump stations.
(a)	The first consideration is to establish the pressure at which the pumps are to operate. On level ground and using the conditions of this example, the differential pressure at Station No. 1 will be 200 pounds per square inch only because there are 10 miles of 4-inch thin wall pipe and 200 barrels per hour being pumped through the pipe. Reference to figure 30 shows that the pressure loss in the pipe is 20 pounds per square inch per mile. If the pipe line extends uphill, however, the same quantity of liquid will not be moved 10 miles with the pump operating at 200 pounds per square inch differential pressure. In part 9 of figure 32, 60 pounds per square inch of the available pressure at the pump is used to lift gasoline and the remaining 140 pounds per square inch is used to overcome friction in 7 miles of pipe.
(b)	A pipe line must be designed and operated so that there is sufficient pressure on the suction side of the pump. When handling gasoline, the suction pressure must not be below 30 pounds per square inch. Lower pressure may cause vapor lock in the system, thus impairing pipe-line efficiency. An exception to this rule will be the pressure on the suction side of Station No. 1, as described in chapter 4 of this manual.
(3)	Solution.
(a)	Place the hydraulic gradient triangle on the profile, figure 29, with the base of the triangle parallel to the datum line of the profile, with zero miles at Station No. 1 (source station), and with the desired pressure graduation on the side of the triangle on the line of the profile. In this example the 200 pounds per square inch graduation, representing the 200 pounds per square inch pressure differential between suction and discharge as desired at Station No. 1, is placed on the line of the profile.
(6)	Draw a light vertical line along the edge of the triangle to the apex and then draw a line along the hypotenuse of the triangle until this line intersects the profile line. On figure 29, the hypotenuse will intersect the profile at a distance of 7 miles from Station No. 1. At this point the pressure on the line will be reduced to the same
32
RATE BARRELS PER HOUR
PRESSURE DROP-POUNDS PER SQUARE INCH PER MILE
Figure 31. Flow of gasoline and water in 6-inch pipe.
33
।
SPECIFIC GRAVITY GASOLINE
0.65	0.70	0.75
■ill
FLOW OF GASOLINE AND WATER j IN 6" ‘PIPE
.based on Fanning's equation
FOR TURBULEN7 FLOW
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NOTE’2.31 FT. HD. WATER	-300	-1000 k---I---X----1"--J
±41000	I LB. PER. SO. IN. |____30Q |qoq|	______________________________
©CONSTRUCT LINES C.B. AND A. B. LOCATING wB TO FORM ANGLE
POINT B.
0	o	<0	BY EXTENDING LINES 0. B. AND 0. A.
20 PSI PER MILE	bx t?[	THE TR,ANGLE Fl6'31 ,S OBTAINED.
£	200 PSI -10 MILES	X?	L,NE ° B- 'NTERSECTING AT 37.9 MILES.
£-»oo	S-ioo	_________________________________
Y° ^’50°	■>	'50° X.	^F HOW TRIANGLE IS USED.
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THIS IS THE RESULTING ANGLE	I MILES	\ MILES
JL	WHEN LOSS IS 20 LBS. PER	0N LEVEL GROUND	SOME OF 200 PS.L
y	pp	MILE.	W,TH 200 RS.I.AVAILABLE USED LIFTING
T I 15 MILES 1,0	\	15	IT IS POSSIBLE TO PUMP GASOLINE UP HILL	M
C.	10 MILES.	(60*STATIC HD.)	M
Procedure for hydraulic gradient triangle.
Figure 32.
34
Figure 33. Finished hydraulic gradient triangle.
35
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-500
-200	X.
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2	X.
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-	o £	\
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-500 p	^X.
" O - h	20 P.S.I. PER MILE
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—600	X.
-2000	\
—700 ~
MILES	X.
5	10	15	20	25	30	35 X.
t______________________1_____________________I_____________________L____________________L______________________I---------------------1_____________________I________X
37.9

STATION NO. 1 CONNECTION IN PARALLEL
UNIT(B)
BELT GUARD
1^" CONDUIT PIPE
1^" CONDUIT PIPE
TOOL BOX
TOOL BOX
CONTROL PANEL
CONTROL PANEL
MAIN LINE
2
HW-3920
SUCTION VALVE
SUCTION VALVE
O
O
O
16-0 DI A.
STORAGE
BELT GUARD —
Ml. MAX. ON LEVEL GROUND
A-737 SAND TRAP
BLANK CAP ON SUCTION
BLANK CAP
PUMP UNIT (A)
A-737 SAND TRAP
BLANK CAP
HW-3797 DISCHARGE HEADER
BLANK CAP ON SUCTION
HW-3797
DISCHARGE HEADER
GATE, CHECK SECTION
GATE, CHECK SECTION
BUDA ENGINE MODEL K-428
WHEN 2 OR MORE TANKS ARE USED PER STATION KEEP TANKS AS FAR APART AS POSSIBLE 600 FEET IS MAXIMUM DISTANCE
HANLON-WATERS TYPE 1626-A G
FIG. 1860-4 ^'x6" GASO PUMP
HANLON-WATERS TYPE 1627
FIG. 1860-4 ^X6" GASO PUMP
NO SDHC 2^ BURGESS EXHAUST SNUBBER
BUDA ENGINE MODEL K-428
NO SDHC 2%"BURGESS EXHAUST SNUBBER
HANLON-WATERS TYPE 1627-A
HIGH SUCTION RELIEF
ENGINE GOVERNOR OIL RESERVOIR
HANLON-WATERS TYPE 1626
SUCTION HEADER
HW-3791	'
HIGH SUCTION RELIEF
SUCTION HEADER HW-3791
HIGH DISCHARGE RELIEF
HW-3920
HIGH DISCHARGE RELIEF
MAKE INOPERATIVE BY SETTING SPRING COMPRESSION HIGHER THAN HIGH SUCTION
RELIEF
ENGINE GOVERNOR
BATTERY BOX /OIL RESERVOIR
TANK FOR
UNIT A)
TANK FOR
UNIT B
36
Figure 34. Arrangement of Station No. 1 (two small reciprocating units in parallel).
. MINIMUM DISTANCE 150'
value as the pressure (30 pounds per square inch) on the suction side of Station No. 1. Station No. 2 is located at this point.
(c)	Station No. 3 and succeeding stations are located in the same manner as Station No. 2 by shifting the hydraulic gradient triangle along the profile, using each station located as a base for locating succeeding stations. The intersection of the hypotenuse with the line of the profile in each case gives the location for a station at which the suction pressure will be the same as for the preceding station, provided the differential pressure (shown on the side of the triangle) is maintained at the designed value.
(d)	Proper location of stations on the line is very important and they should be located on the ground as near the point indicated on the profile as possible, so that the desired pressure gradient may be maintained in the pipe-line system.
(e)	The hydraulic gradient triangle can also be used to determine the actual pressure which will be on the line at any desired point when there is flow. Without flow, the friction loss in the pipe, of course, does not exist and only the scale of pounds per square inch on the triangle is used.
c. Other Considerations in Pipe-Line Design. There are many other consideration in the design of a pipe-line system. Some of these are discussed in the following paragraphs as a continuation of the design example for a 4-inch spiral weld line to carry gasoline. Reciprocating pump stations along this line and the pressure regulation stations on the downhill grades are to operate automatically.
(1) Station No. 1 has two pumping units, one of which is a stand-by connected in parallel on the line at the same place hydraulically (fig. 34). The requirement that the two units be at the same place hydraulically means that each unit should be installed at approximately the same elevation, even though they are a considerable distance apart. Station No. 1 sets the rate of pumping for the whole system. It is important, therefore, that the two pumping units be placed at Station No. 1 to be certain that the station can pump into the line under all conditions.
(a)	The differential pressure controls on Station No. 1 are adjusted to hold a maximum differential pressure of 200 pounds per square inch on the line between Station No. 1 and Station No. 2 (230 pounds per square inch discharge at No. 1). This 200 pounds per square inch differential pressure sets the rate at which liquid will flow in the line.
(6)	The high suction relief valve at Station No. 1 will be set so that it opens at 250 pounds per square inch. Connection to the diaphragm will be made from the discharge manifold. The double port opening of this valve is large enough to return the full capacity of the pump to the storage tanks. Connection to the tanks is made into the suction line behind the check valve between the tanks arid the pump. The connection to the high discharge relief diaphragm will be plugged so that it stays closed.
(c)	The low suction controller at Station No. 1 is set to control at 30 pounds per square inch if the suction pressure at this station is supplied by a booster pump operating on a storage tank. If the suction pressure at Station No. 1 is due to head of liquid in storage tank only, the low suction controller must be made inoperative and the station placed on manual control. This controller is not, in general, sufficiently sensitive to respond properly to small variations in pressure such as that brought about by change in the fluid level as liquid is withdrawn from a tank. Manual operation of the pump will necessitate maintaining an accurate check on tank gages at all times while pumping.
(2) (a) Station No. 2 is another two-pumping-unit station, one unit of which is a spare. Station No. 1 can pump no farther than Station No. 2 with its maximum discharge fixed at 250 pounds per square inch and the continued delivery of liquid through the line will depend upon Station No. 2 being operative at all times. The two pumping units should be located at approximately the same elevation, not over 1,000 feet apart, and connected in series (fig. 35).
(b) Station No. 2 differential pressure controller is adjusted for 300 pounds per square inch. With Stations No. 1 and No. 2 at the same elevation and no flow in the line, the suction pressure at Station No. 2 is 250 pounds per square inch. If Station No. 2 is at an elevation greater than that of Station No. 1, the suction pressure at Station No. 2 with no flow will be reduced by the difference in static head between the two stations. With this maximum suction pressure of 250 pounds per square inch, plus 300 pounds per square inch differential setting, the maximum discharge pressure and the setting of the high discharge relief valve will be determined. When Stations No. 1 and No. 2 are at the same elevation, or when Station No. 1 is located at a higher elevation than Station No. 2, the high discharge relief valve setting will be 550 pounds per square inch.
37
(3)	Stations Nos. 3 and 4 are located only 150 pounds per square inch pressure differential from Station No. 2 and Station No. 3, respectively. This is required because:
(a)	The high discharge reliefs at Stations Nos. 3 and 4 are set at 650 pounds per square inch maximum.
(b)	Differential pressure controllers are set to control at 300 pounds per square inch differential pressure. With Stations Nos. 3 and 4 located only 150 pounds per square inch remote from Station No. 2 and Station No. 3, respectively, either one of these stations could be out of operation and normal flow maintained. Both Stations Nos. 3 and 4 cannot be down at the same time and have the line maintain its 200 barrel per hour capacity rate without overtaxing Station No. 2 with 500 pounds per square inch differential pressure. The differential pressure controller is used to insure that the engine of a pumping unit is not overloaded,
(c)	When neither Stations Nos. 3 nor 4 are operating the spare unit at No. 2 should be started and the two units operated in series with 250 pounds per square inch differential pressure across each station. This is necessary because there is 150 pounds per square inch pressure loss between Stations Nos. 2 and 3, 150 pounds per square inch between Stations Nos. 3 and 4, and 200 pounds per square inch between Stations Nos. 4 and 5, a total pressure loss between Stations Nos. 2 and 5 of 500 pounds per square inch. A balancing pressure would be developed at Station No. 2 by operating both units there in series, as above outlined.
(d)	Stations Nos. 2 and 3, and Nos. 3 and 4 can be only 150 pounds per square inch apart, because Station No. 2 is limited by its differential pressure controller to 330 pounds per square inch discharge pressure. Therefore, Station No. 2 is capable of pumping to Station No. 4, when Station No. 3 is out of service.
(e)	The high discharge relief valve at Station No. 3 is set at the maximum discharge pressure of Station No. 2, plus 300 pounds per square inch differential setting, less the static head between Stations No. 2 and No. 3 when Station No. 3 is at a higher elevation than Station No. 2, but not to exceed 650 pounds per square inch. The high discharge relief valves at all stations beyond Station No. 3 are set at 650 pounds per square inch, except in the special cases discussed elsewhere in this chapter, thus allowing a maximum operating discharge pressure of 630 pounds per square inch when required.
(4)	All other stations are located at 200 pounds per square inch differential pressure spacings.
(5)	Figure 36 shows the hydraulic relationships of stations by means of a hydraulic gradient when various stations are out of service. In normal operation Station No. 1 has a discharge pressure of 230 pounds per square inch. Stations Nos. 2 and 3 each have discharge pressures of 180 pounds per square inch, and all stations beyond No. 3 have discharge pressures of 230 pounds per square inch. It should be noted that all pressure values shown in Figure 36 must be increased by 30 pounds per square inch, since minimum suction pressure at the pumping station has arbitrarily been assumed as 30 pounds per square inch. When one or more adjacent intermediate stations in a given pipe line are not operating, the increased load on the station immediately upstream is spread over the upstream stations, thus distributing the additional load uniformly. This is accomplished by the operation of the differential pressure controller which limits the differential pressure between suction and discharge on any station to 300 pounds per square inch.
(a)	For example: Consider that Station No. 5 is not operating. Station No. 4 must discharge at 430 pounds per square inch to reach Station No. 6; therefore the suction pressure at Station No. 4 must reach 130 pounds per square inch and Station No. 3 must discharge at 280 pounds per square inch so that the suction pressure of 130 pounds per square inch can be maintained at Station No. 4. Station No. 2 is not affected since Station No. 3 can work against 300 pounds per square inch differential pressure if necessary.
(b)	Suppose Stations Nos. 6 and 7 are not operating. Station No. 5 must discharge at 630 pounds per square inch to reach Station No. 8 which of necessity increases the suction pressure at Station No. 5 to 330 pounds per square inch, and Station No. 4 must discharge at 530 pounds per square inch to maintain 230 pounds per square inch suction pressure at Station No. 5; since Station No. 4 is only 150 pounds per square inch away from Station No. 3, the discharge at Station No. 3 is raised to 380 pounds per square inch to maintain a 230 pounds per square inch suction pressure at Station No. 4 and Station No. 2 must discharge at 180 pounds per square inch to maintain a suction pressure of 30 pounds per square inch at Station No. 3.
(c)	The hydraulic gradient diagram in figure 36 shows that normally no more than two adjacent
38
stations can be out of operation at the same time, and still maintain the desired rate of flow. Furthermore, if two adjacent stations are not in operation, the first four stations immediately upstream must be pumping to maintain operation at the designed rate. An illustration of pumping at a reduced rate in a pipe-line system, due to three adjacent stations not being in operation, is brought out by the following example: Assume a 20-station pipeline system, with Stations Nos. 9, 10, and 11 not in operation, and with a static head of 80 pounds per square inch between each station. This condition would require that Station No. 8 pump all the way through to station No. 12. The maximum allowable discharge pressure at station No. 8 is 630 pounds per square inch and the assumed suction pressure at Station No. 12 is 30 pounds per square inch. The available pressure for pumping liquid from Station No. 8 to Station No. 12 is, therefore, 600 pounds per square inch. Total static head between Station No. 8 and Station No. 12 is (80 times 4) 320 pounds per square inch, which leaves 280 pounds per square inch to be consumed as friction loss over the distance of 24 miles between Station No. 8 and Station No. 12. This represents a pressure loss due to friction of approximately 11.7 pounds per square inch per mile. Reference to figure 30 shows that a pressure drop of 11.7 pounds per square inch per mile in a 4-inch pipe line with gasoline of a specific gravity of 0.70 gives a rate of about 155 barrels per hour. . This rate can be maintained with Stations Nos. 9, 10, and 11 not in operation.
(d)	In case three or more adjacent stations are out of service the first upstream station will reach a pressure at which both the high discharge and high suction relief valves will open and the pump speed will be reduced to idling. This idling condition will prevail until the first downstream station which continues to pump pulls the line pressure down to such a value that the idling upstream station resumes pumping. After building up to the maximum predetermined discharge pressure, the upstream station will again bypass and slow down to an idling speed. This intermittent operation will continue until a sufficient number of stations have resumed pumping to permit the system to operate at the designed throughput of 200 barrels per hour.
(6) Steep uphill gradients. In pumping liquid over a steep uphill grade requiring more than one station where pressure reducing regulators are used on the downhill side to control pressure, it is nec
essary to place a standby pumping unit at the foot of the downgrade for the same reasons that one was placed at Station No. 1. The downhill line is equivalent to the storage tanks at Station No. 1, inasmuch as a limited suction pressure is available due to the action of the reducing pressure regulators. All successive stations should be spaced at the usual 200 pounds per square inch pressure intervals along the line.
(7) Pump station locations on hill crests. A pump station should not be placed at or near the crest of the hill shown, for example, on the profile in figure 29 at mile 72. The downhill slope beyond mile 72 is so steep that no pumping is needed. In the example illustrated in figure 29, two stations should be installed between the double pump station and the top of the hill to prevent the two-unit station from operating continuously against a high discharge pressure.
d. Use of pressure-reducing regulators. Pressure-reducing regulators are used to protect pipe on downhill grades from excessive pressures which are developed where static pressures greatly exceed friction losses.
(1)	Normally, these regulators should be adjusted to reduce the pressure to 50 pounds per square inch on the downstream side and are spaced 200 pounds per square inch pressure differential apart. One regulator can be used for a 400-pounds-per-square-inch differential, but it is recommended that they be spaced at not more than 200 pounds per square inch apart when a series of them is required.
(2)	The regulator is constructed so that failure of the diaphragm will allow the valve to open wide, with only the valve orifice restricting the liquid flow. This restriction would probably be enough to prevent the pressure from becoming excessive under flow conditions, but if a shut-down of the line occurred downstream from the broken regulator the line would not be protected against excessive static pressure.
(3)	The Hydraulic Gradient Triangle should be used to locate both pump and pressure reduction stations all along the profile. There may be a condition when the profile and the hydraulic gradient (hypotenuse of the triangle) approximately coincide. When this is the case, both flow and static conditions should be investigated. In general, it is safe to locate pressure reduction regulators on the profile with the scale of pounds per square inch on the Hydraulic Gradient Triangle. This procedure is as follows:
(a)	Place the zero point of the vertical scale of
39
BATTERY BOX ENGINE GOVERNOR	BATTERY BOX ENGINE GOVERNOR
NO SDHC 2^" BURGESS ,—1	OIL RESERVO,R	NO SDHC 2pBURGESS _ X / OIL RESERVOIR
EXHAUST SNUBBER	45/1	EXHAUST SNUBBER
BUDA ENGINE	/	I BUDA ENGINE
K 1 PUMP ;! ® ^MODEL K-428	|[ 1 PUMP !; U ^MODEL K-428
OC1T	' ib UNIT (A) !!	I [\ UNIT(B) !■
BELT GUARD । , L-rv- <4,	, u	BELT GUARD 1 L 3. «
CONDUIT PIPE	BtLI UUAK}^| i t~~	1 CONDUIT PIPE
FIG. 1860-4 ^"x6" I [/ I --'—4 .—-TOOL BOX	FIG. 1860-4 X 6" I \l~ZZ “1L.—-TOOL BOX
GASO PUMP. j iH _JJ___■	GASO PUMP } jU—. —JJ i
I	!	| /CONTROL PANEL	' ||	CONTROL PANEL
J__K HANLON WATERS	I jf HANLON-WATERS
suca^”. Wia tyx2>h,gi^tion	suTwn3ycMa	type 'r>H,GHRsTioN
T	HhW-3920	IJhW-3920
/LR	HW-3920	H	HW-3920
A-737	/ j tIJ—A-737	/	/ nu-A;---9
SANDTRAP-^.	/ ^^7	\	SAND TRAP_	/	f	\
HW-3797 7	/ HANLON-WATERS	X	HW-3797 7	/ UAmi^m watcoc
DISCHARGE HEADER / TYPE 1626-A	DISCHARGE HEADER / HAt!?CNi*^T|RS
/	/	IT Pt lo26”A
HIGH P’^CHARGE	H|GH DISCHARGE
PI--p,	RELIEF	a——D	RELIEF
HW-3731	IJ	HW-3731
DISCHARGE LINE x NOT OVER 1000 ON JT	DISCHARGE LINE^
rA	j_g LEVEL GROUND T I,	~£I
(gk-SUCTION VALVE DISCHARGE VALVE-kW	(HL-SUCTION VALVE DISCHARGE VALVE
UP-STREAM A FLOW	H	UP-STREAM H FLOW
IE J L -	g n XL JSXagS- ------------------------Oja
/	DOWN-STREAM	MAIN LINE	DOWN-STREAM
duudimc iimit	CHECKVALVE	ONE UNIT OPERATES AT A TIME HW-3793 CHECKVALVE
PUMPING UNIT BYPASS SECTION	BYPASS SECTION	PUMPING UNIT
(SMALL)	(SMALL)
Figure 35. Arrangement of Station No. 2 (two small reciprocating units in series').
40
HYDRAULIC GRADIENTS : PRESSURES AT VARIOUS RECIPROCATING PUMP STATIONS
41
POUNDS PER SQUARE INCH ’
| STATION _ . _ _ _ _	2 '3 -4 -5 -6 ~7 -8	9 ________ I - 2 :3 :: 4	~5 ::6	7	8	9-10 11-1213 14

■ 'z W
LOCATION OF TANKS AND DISPENSING STATIONS
SCHEMATIC LAYOUT - NO SCALE
SITE OF AIRFIELD
P
LOCATION CLOSE TO MAIN LINE
Underground Tanks
Block Valve
WOODED AREA
O
DISPENSING SECTION
Deep Well Pumping Unit (one per tank) Used to Supply Airfield Pumping System
TERMINAL TANKS (near Road or R.R.)
FLOW a
PUMP
BLOCK VALVE
-I PUMP
Figure 37. Schematic layout of tanks and dispensing stations along a main pipe line.
BLOCK VALVE As close as possible To Main Line
K AUXILIARY
LINE TANK
To Advanced Bases
Reducing Regulator
STATION NO. 11
REDUCING REGULATOR

Highway
? STATION
NO. 10
MAIN LINE
7 to 10 Miles between Stations
200 Differential
LOCATION
AWAY FROM MAIN LINE
£ ,0

42
BRANCH LINES
.SCHEMATIC LAYOUT - NO SCALE
FROM STATION NO. 1
LINE STORAGE TANK
STATION NO. 11

STATION NO. I 2
Station No. 11-1
Form
PUMP-
COUNTRY ROAD
STATION NO. 13
To Advanced Bases
- BLOCK VALVES
Terminal Storage Tanks
\ Short
Branch Line
Main Line
7 — 10 Miles between Station
200 # Max. Differential
STATION NO. 10
Station No.1V!
Branch Line
7 to 10 Miles between Stations
200 # Max. Differential
BLOCK VALVE
REDUCING REGULATOR
PUMP-*
BASE
DISPENSING SECTION
Pipe Line 7 to 10 Miles
Long, Differential
200 # between Station
No. 11 and Station No. 11 — 1
Church
Yard
Station No. 113
Figure 38. Schematic layout of a branch line.
43
c A


the Hydraulic Gradient Triangle at the point representing the top of the hill on the vertical profile. The base of the triangle should be horizontal. Mark on the profile paper the 200 pounds per square inch point and extend this point with a line drawn horizontally until it intersects the profile. This is the location of a pressure reduction regulator. Succeeding regulators are located in a similar manner (fig. 29).
(b)	This method considers only the static pressure between stations and should be used to prevent the building up of excessive static pressure under “no flow” conditions. If the gradient method of locating stations is used, there is a possibility on long downhill slopes that the hydraulic gradient may be parallel to the ground slope. This condition would not require the use of reducing regulators under flow conditions, but under static conditions it would be possible to build up excessive pressure. Where friction loss is greater than static head, a regular pumping unit would be installed in the usual manner.
e.	Large reciprocating pumps equipped with 4- by 10-inch liners operate at 400 pounds per square inch differential pressure while pumping 200 barrels per hour through a 4-inch pipe line and with stations spaced at twice the normal distance for the small reciprocating pump service. It is for this reason a station cannot be bypassed as a pressure of 800 pounds per square inch would be developed and this value is greater than the allowable working pressure recommended for the equipment.
f.	Use of Check Valves.
(1)	Check valves are used in the line to prevent back flow of liquid when upstream pumping units are not operating, or when the uphill line is broken at some point. These valves are especially neces
sary on long uphill lines. They have no use on downhill lines.
(2)	It is good practice to place a check valve section in the main line at the discharge side of each station. This prevents the backing up of liquid in the pump when the system is shut down and makes it easier to resume pumping operations.
g.	Use of Block Valves.
(1)	Block valves are used to isolate pump stations and sections of the line during repair in the event of breakage, and also to divert the flow into branch lines. A block valve should be placed in the line at intervals of approximately 1 mile. Concealed locations should be used wherever possible, and they should be reasonably accessible in case it becomes necessary to close the valve for any reason.
(2)	The section of line most vulnerable to enemy action and natural destructive forces should be well protected with block valves.
h.	Location of Dispensing Station. Dispensing stations will be located along the pipe line as required for tactical operations. It is anticipated that storage tanks will be provided for the dispensing stations and fluid may be withdrawn from the line at any point where the pressure is sufficiently high to cause flow into the tanks. Reducing pressure regulators will be provided to reduce pipe-line pressure to values around 10 or 15 pounds per square inch for delivery into products storage. The reducing pressure regulators can be adjusted to provide higher delivery pressures if required.
i.	Branch Lines. Pipe-line distribution systems may be more extensive than a simple line connecting a supply with a single point of distribution. Branch lines, the operation of which is outlined in this manual, may be used in a wide variety of ways as required. Figure 38 shows a schematic layout of a branch line.
44
CHAPTER 4
CONSTRUCTION
11.	PREPARATION OF RIGHT-OF-WAY.
a.	Military pipe lines should always be laid out along a course which provides the maximum concealment. Benefits of this precaution will be lost, however, if the right-of-way is not prepared with a minimum of disturbance of natural cover. Obstructions such as small brush will be an inconvienience in laying the line but nonetheless should be left undisturbed so far as possible. Major obstructions, such as steep cliffs, large boulders, and deep ravines should be avoided, whenever possible.
b.	Grading and leveling the right-of-way is not necessary. Flowing streams should be crossed by utilizing existing bridges. If none are available, simple suspension bridges of the type shown in figure 39 should be constructed.
12.	INSTALLATION OF COMMUNICATION SYSTEM. As soon as the course of the projected pipe line has been determined and the right-of-way prepared, a telephone or telegraph line should be installed along it for communication during the pipe-line construction period and for dispatching purposes when the pipe line is in operation. Alternative systems of communication are radio and messenger.
13.	PRIMARY DISTRIBUTION OF PIPE. Pipe, couplings, and miscellaneous fittings will be received at beach or rail head, (fig. 40) depending upon the location of the projected line. The primary distribution of the pipe should be to stock piles at about 20-mile intervals where road net permits stringing of pipe by truck. Pipe should be transported from stock piles to the right-of-way by truck or truck-drawn trailer. Over rugged terrain where manual stringing is necessary, stock piles should be established at shorter intervals, at points where trucks can reach the right-of-way. A Type I, two-wheel, utility pole type trailer, equipped with two load
binders, drawn by a 2K-ton 6 by 6 truck, or other suitable prime mover has been found satisfactory for this service. The maximum permissible load for the trailer is approximately fifty 20-foot joints of light weight 4-inch pipe (4,500 pounds) on average dry dirt roads. (See figs. 41, 42, and 43 for examples of this equipment in use.) Trucks of conventional oil field design are being built for use of the pipe-line detachments (fig. 44). These trucks will be 2 ^-ton 6 by 6 prime movers, with rear mounted winch, flat bed, detachable A-frame. Such trucks may be used also for hauling the pumping units and spotting them.
14.	STRINGING PIPE AND COUPLINGS.
a.	Pipe in stock pile which shows pronounced rusting should be thoroughly swabbed with wire brush cleaner provided for this purpose and swept with compressed air before it is strung along the right-of-way for laying. Extreme care should be exercised when coupling the pipe in the field to guard against dirt and other objectionable particles being left in the completed line.
b.	Since the pipe is lightweight, it can be strung by a two-man crew unloading from a slowly moving truck (fig. 45). Pipe must be distributed with care and laid end to end so that lengths will not have to be carried along the line by the coupling crews. This will also eliminate extra trips by the trucks to supply additional pipe at points where the stringing crew has already passed.
c.	Couplings should be strung from a separate truck. One coupling, complete with bolts and gasket assembled, is laid out at each joint along the entire line (fig. 46). At least 15 percent more couplings than are actually necessary to connect the line should be on hand for replacements in the event of failure of any couplings after the line has been tested. They should be held in stock by the maintenance and repair crew at convenient locations along the line.
45
552517 0 - 43 -4

RIVER CROSSINGS
SCHEMATIC, LAYOUT - NO SCALE
Select Sturdy mature trees well rooted
10'0
BLOCK VALVE
BLOCK VALVE
SUSPENDERS
PIPE LINE
ANCHOR
Guy Wires
SUSPENSION LINE
BLOCK VALVE
LOOP
PIPE LINE SUSPENDED FROM TREES
Guy Wires
SUSPENDER
JOINT
LOOP
PIPE
SUSPENSION LINE
PIPE LINE
G	a-
weldedpipe	nrFwrmi
Figure 50. Detail drawings of pipeliner's jack and lazy board.
54
line, will span 650 feet without intermediate support with a safety factor of four. All spans must be anchored firmly at each bank or cliff, as the reciprocating pumps used cause a pulsation, the repeating action of which may result in fatigue failure of the pipe.
b.	One valve section should be installed on each side of a crossing.
c.	The general rule for sag in cable is 10 feet per 100 feet of span.
17.	INSTALLATION OF RECIPROCATING PUMP STATION. Pump station sites should be chosen with a view of concealing the equipment by taking advantage of any natural cover that is available. The site chosen must be firm, level ground, large enough to permit the wide dispersal of all the equipment included in the installation.
a.	The site for the pumping unit or units should be leveled. Pumps should be set on a wood-beam base, if possible, otherwise it must be set on solid ground. Filled ground is unsuitable for a pumping unit. Leveling up a pumping unit is important, since the proper functioning of the unit depends upon having the machinery level. For this purpose use a spirit level.
b.	Procedure for Leveling Pumping Unit.
(1)	Block up the skid frame on substantial timbers (6 inch by 6 inch or 8 inch by 8 inch) if available, so that the unit is nearly level and at the desired distance from the main line.
(2)	With a spirit level placed on the pump skid, or a machined surface which can be used as a datum, level the unit in both directions by using wood or steel wedges or bars. The suction and discharge flanges of the pump then can be checked for plumb. A slight variation from plumb will be compensated for by the Victaulic couplings.
(3)	Having leveled the unit in this manner, replace the temporary blocking with permanent blocking. If materials are available and time allows, pour a concrete foundation for the engine and pump, and anchor the skid frame to this base, with anchor bolts through the holes in the skid frame. Blocking is also required under suspended valves, relief valves, sand traps, and other unsupported parts.
c.	Alinement of Pump and Engine, and Belt Drive.
(1)	Use the adjusting screws on the skid frame that bear against the engine base plate to increase or decrease the spacing of the engine from the pump (fig. 59).
(2)	Use a straightedge or string to aline the motor with the pump. A straightedge placed along the
side of the driving sheave on the engine and along the side of the driven sheave on the pump should touch both sides of both sheaves at the same time.
(a)	When the straightedge touches only one edge of the drive sheave and one edge of the driven sheave, the motor must be shifted in the proper direction toward or away from the front of the engine. This is done by means of the two adjusting screws at the base of the motor.
(b)	Draw the adjusting screws up snugly to prevent any shifting in this direction while the drive belts are being adjusted.
(3)	Belt adjustment.
(a)	Check the tension of the belts after their installation by pressing down on them with the hand. It should be possible to depress each belt from 1 inch to 1% inches when they are in proper adjustment.
(b)	If the belts are too tight, the engine must be moved toward the pump in order to relieve the belt tension. This is done by use of the adjusting screws on the bed plate, being careful to maintain the alinement of the drive sheaves.
(c)	If the belts can be easily depressed more than 1% inches, or if they seem to be hanging loosely on the sheaves, they need to be tightened. This requires that the motor be moved farther away from the pump.
(d)	When the belts have the right amount of tension and the sheaves are alined, the adjusting screws should be securely locked in place with the lock nuts provided. The engine and pump mounting bolts should then be securely tightened to the skid frame, to prevent any movement of one unit relative to the other, and a final check made for alinement and level.
d.	Installation of Station Header Piping. (1) When the engine and pump are properly set and alined, connect the station header piping to the pump and to the main line.
(2) The station header assembly consists of specially cut lengths of pipe, ells, flanges, valves and relief valves. Each section of pipe of this assembly as shipped from the factory has a part number stenciled on it corresponding to the numbers shown on the drawing.
(a)	The station bypass section is installed in the main pipe line by removing the plain pipe section where it is desired to locate the station. The station bypass section is installed with the check valve set so that the discharge pressure will close it against the lower suction pressure. The check valve must open to allow fluid to bypass the station when the station is inoperative.
55
Figure 51. Placing gasket on pipe end.
Figure 52. Gaskets should be placed flush with pipe end.
56
Figure 53. Preparing pipe joint for alinement. The end of the assembled pipe line is on the lazy board.
Figure 54. Slipping gasket over ends of pipe.
57
Figure 55. Placing bottom and top halves of coupling over the gasket
Figure 56. Holding coupling in place while bolting it together.
58
Figure 57. Turning the nuts down evenly.
Figure 58. Completed coupling. _
59
Figure 59. Location of adjusting screws to facilitate sheave alinement.
60
(b)	Install the pumping unit adjacent to the main line whenever practicable.
(c)	In the usual installation the sand trap section, with suction valve and discharge valve sections, are connected to the bypass section with an L coming out of the top of the main line pipe.
(d)	All connections between the various pipe sections are made with Victaulic type couplings.
(e)	Connection of the piping to the pumps is by means of flanges which are fabricated with adapter nipples for connection with Victaulic type couplings.
(/) Make flange connections according to the following procedure:
1.	Clean the surface of the flanges to remove all grit and other foreign material.
2.	Place flange halves together loosely, using the studs or bolts that are provided. Loosely engage the two bottom bolts and the next two bolts above these but below the center line of the flange.
3.	Place the gasket into proper position on the raised faces of the flanges.
4.	Check the flanges for alinement by centering the inside of the pipe with the port on the pump. 5. Tighten two diametrically opposite bolts first, then two opposite bolts 90° from the original two. Work around the flange tightening opposite bolts until the flange is pulled up evenly.
6. Check the tightness of all bolts again.
(£) When space is not available, it is not imperative that the pumping unit use the standard type of installation shown in fig. 60. A compact hook-up, shown in fig. 61, can be used. In this layout the station pump and engine are inclosed inside the piping of the station, the whole station occupying an area of 20 by 24 feet, whereas, in the standard installation an area of approximately 20 by 34 feet is required. In the event it is desired to pump backward through the line, the hook-up shown in figure 62 is suggested as a quick method of changing the direction of flow. The check valves and the piping must be reversed on all stations along the line before pumping is started. A thorough check must be made of the hydraulic design of that portion of the system through which it is proposed to reverse the flow as uphill and downhill gradients become reversed.
18. STORAGE TANKS.
a. Select tank sites to take full advantage of available natural cover. Tanks should be set on hillsides, if convenient, so that the tank installation may be pitted. (See illustration of typical tank pit installation, fig.63.) A hillside tank site
has the additional advantage that it furnishes a positive gravity feed to the pump or dispensing stations located below it.
(1) If pump intake pressures are too low, gasoline will vaporize and cause a reduction in liquid pumping efficiency or even complete vapor lock of the pump. This gasoline vaporization can only be eliminated by maintaining a pressure in excess of the gasoline vaporizing (boiling) pressure throughout the system from storage tank to the lowest pressure point at the pump.
(2) Where gravity feed from tank to pump is to be employed there is a minimum elevation which a tank must be above a pump. This minimum elevation can be calculated for centrifugal pumps by adding pump entrance pressure loss constant to friction pressure loss for maximum liquid flow rate between tank and pump, and by converting the resultant total pressure from pounds per per square inch to feet of liquid head units. Reciprocating pump entrance pressure loss is more than equalized by suction effect, the net result being that gasoline can be “lifted” as much as 6 to 10 feet. In no case, however, should a reciprocating pump be located at an elevation above the supply tank outlet, as a positive prime must be maintained at all times.
(a)	Pup centrifugal pump entrance pressure loss constants for maximum flow rates and minimum gasoline specific gravity are 2.2 and 4.9 pounds per square inch for 4- and 6-inch pipeline service, respectively.
(6)	Figure 64 shows pipe friction loss for various lengths of 4- and 6-inch pipe transmitting 200 and 400 barrels per hour of maximum specific gravity gasoline, respectively. Figure 65 shows the frictional effect of pipe fittings expressed in terms of equivalent straight pipe. The total equivalent length of pipe for the pipe fittings between tank and pump should be added to the actual pipe length to obtain the maximum flow rate friction pressure loss from figure 64.
(c)	Example. A tank is located 600 feet from a centrifugal pump. Gravity feed of 0.68 specific gravity gasoline through a 4-inch pipe from tank to pump is required. There are six ells in the line which, from figure 65, have a resistance to flow equivalent to 10 feet of straight pipe each, or a total of 60 feet. Add 2.2 pounds per square inch pump entrance pressure loss and 3 pounds per square inch friction pressure loss for the 660 feet of equivalent pipe, giving a total of 5.2 pounds per square inch. Convert to feet of head by multiply -
552517 0 - 43 -5
61
Figure 60. Standard small reciprocating unit installation.
62
PUMPING UNIT, SMALL (COMPACT HOOK UP)
HW-3793
A-737
BELT
GUARD
NO, SDHC 2? BURGESS
EXHAUST SNUBBER BATTERY BOX
HW-3791
HW-3920
HW-3797
FIG. 1860 4^X6 GASO. PUMP
TOOL BOX

HW-3731
CONDUIT PIPE
CONTROL PANEL
BUDA ENGINE MODEL K-428
HANLON-WATERS TYPE 1627-A
ENGINE GOVERNOR OIL RESERVOIR
HANLON-WATERS TYPE 1626-A
HW-3920
Figure 61. Compact arrangement for small reciprocating unit.
63
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54
SUGGESTED INSTALLATION OF STORAGE TANKS IN P
. ____________ y
gauge mesh
’	SCALE 'E" ~/'O"	FOR CAMOUFLAGE
GASOLINE TANK
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1^222-J INSTALL VAL VE ON 8GASOUNE	DOWN TO DESIRED DEPTH
B* GASOLINE	LINE SO THAT HAND WHEEL
MAINS	IS ABOVE GROUND
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FOK WCLOtNG T	X|W I \	-R-» "GASOLINE MAIN~G	b’ DRAIN f	____?	 inches high by approximately 60 inches wide, and all bolt together with synthetic rubber strip gaskets between the laps. Photographs illustrating the preparation of foundations and erection of tanks show details. The drawing which accompanies each tank must be studied. It will show the number and arrangement of interchangeable parts.
(a)	Tank foundation. Firm graded dirt is a satisfactory tank foundation for almost all conditions. A concrete pad or spread foundation is not warranted. Where the ground is moist and subsoil drainage poor, a pad of uniformly sorted gravel makes an excellent foundation. Level ground with a sweep (fig 66) attached to a stake driven in the center of the tank location. By using a carpenter’s level on the sweep the ground can be dragged level. The leveled area should be 2 feet larger in diameter than the tank. 7 he tank deck will not fit unless the tank bottom
66
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Nature of Resistance
Figure 65. Resistance of fittings.
68
— a/D -- '/A L"-d/D • W ---fb 1 54
Water -A
Steam and Gases
is level. If the ground is corrosive (sour) a 2-inch layer of clean sand or gravel, or a sheet of tar paper spread over it, will protect the tank bottom.
(6)	Tools. Two sets of field erection tools are furnished with all tanks of 500-barrel capacity and greater, and one set with each 100- and 250-barrel tank. Each set consists of—
3 speed wrenches.
5 ’/z-inch short sockets.
4 ’/rinch long sockets.
3 5/8-inch by 12-inch drift pins.
3 5/8-inch by 18-inch drift pins.
3 8-inch crescent type adjustable wrenches. 2 deck rope hooks.
2 5/8-inch by 6-inch flat cold chisels.
2 5/8-inch by 6-inch diamond point chisels.
2 14-pound ball peen hammers.
24 patch bolts.
2 3-inch flat paint brushes.
1 Ampco metal No. C-3 flat caulking tool, and
1 Ampco metal No. H-3 ball peen hammer.
Some of these tools are shown in figure 67.
(c) Bottom section. All sizes of tank bottoms are made up of pie-shaped segments assembled around a circular center plate. There are two rows of segments in the 5,000- and 10,000-barrel tanks. The center plate of the 10,000-barrel tank is in two halves.
1.	Spread out all pieces of the bottom section in approximate position on the foundation (fig. 68). If the center piece is in two halves, bolt them together with a bolt-head retaining channel on the underside and a strip of punched gasket between the halves. The channel must not cover the end holes, but the gasket must extend all the way from end to end of the seam. Use countersunk or recessed nuts or washers and Neoprene ring washers throughout the bottom-section assembly as a precaution against leakage around the bolts.
2.	The outer gasket for the circular center plate is furnished unpunched. To install this gasket place a strip of plain gasket over the circumferential holes and punch down through it with a drift pin, rolling the pin around several times to clear the hole. Place one short channel on the underside of each hole; and use %-inch by 1%-inch bolts. String a strip of straight gasket from bolt to bolt, pressing it down firmly over each bolt after a hole has been punched through it. The puckers in the gasket will not prevent making a tight joint. Center plates of the small tanks are fabricated to
hold bolt heads so that bolt-head channels are not needed; and gaskets are furnished in three pieces cut to a circle. A molded chime lap gasket is placed flat side up beneath the circumferential strip gasket at each bottom plate seam. When more than one single piece of gasket is used, the pieces must be spliced by overlapping them the distance between two bolt centers (fig. 69).
3.	Fasten each inner pie-shaped piece to its outer pie-shaped piece in the same manner the two halves of the center plate were fastened. The outer piece laps over the top of the inner piece; the bolthead retaining channel must not cover the holes at either end; but the gasket must extend from end to end of the seam.
4.	Place strips of punched gasket on both edges of the starting segment (fig. 70). Note that the inner part channels are not the same length as the outer part channels. Keep the innermost end of the inner channel clear of the hole which will lap over the bottom center plate; keep the outermost end of the outer channel clear of the chime hole; and extend the gasket a bit beyond both ends of the seam (fig. 71).
5.	Place a strip of punched gasket on the righthand (looking at the center plate) edge of each pie-shaped piece after having first placed a bolthead channel underneath the edge of the plate with the bolts in place. A loosely placed nut on a bolt at each end of the channel will hold the channel in place, but these nuts must be removed before the plates are laid together. Work around the bottom in a counterclockwise direction to the last pie-shaped piece. The last plate will lap on top at both edges. The bottom is now assembled.
6.	To bolt the bottom plates together slide a 1- by 4-inch board under each edge of the starting segment (fig. 72). Take off the nuts which had been used to hold the bolt-head channel in place. Insert a molded chime lap gasket, smooth side down, under the right-hand edge of the segment where it laps over the center plate. Pick up the next bottom segment to the right (counterclockwise direction) and set its left-hand edge holes down easily over the right-hand edge of the starting segment, starting at the inner end and working out. Spin all of the nuts onto the bolts loosely. Use only the special countersunk or recessed nuts or washers with accompanying Neoprene ring washers. Pick up the right-hand edge of the last bottom segment laid, pull out the 1- by 4-inch plank from under the left-hand edge and re-lay it under the right-hand edge (fig. 73). Continue around the tank bottom in this manner.
69
Figure 66.
Figure 68.
SCAFFOuO BRACKET
*	DECK ROPE HOOK
PATCH BOLT	wtHW., -p_- .■■■■■,.■■■■■■■■ ,„,—^
S«ORT OR ITT Pin
LONG OR If T PIN
"t- /^ar^WBex
J^/	& [ M)
SJ&S	£NC SHORT SOCKET i SPEEO FRENCH
WRENCH
a.....—..............................TBLga.
LONG SOCKET
Figure 69.
70

Figure 67.
Figure 70.
Figure 71.
Figure 73.
Figure 72.
71
The last segment to finish the tank bottom will overlay on the top side at both edge overlaps. All of the 1- by 4-inch boards should be removed from under the tank bottom, when the last segment has been laid.
7.	Before tightening all the bottom bolts (see that only the countersunk or recessed nuts or washers have been used on these bolts), the tank assemblers should experiment to determine just how tight they should be. If the bolts are too tight, the gasket will be crushed away from the bolts and the tank will leak; if they are too loose, the tank will leak. Tighten the bolts until the gasket just begins to push out at the edge. Take the first seam apart after tightening it to make sure that the gaskets have not been crushed and that the right amount of force was used in tightening the bolts. When this has been determined, all of the tank bottom bolts should be tightened (fig. 74).
8.	Block up the edge of the bottom with 4- by 4-inch blocks, so that the chime bolts can be inserted (fig. 75). Bolt head channel irons are not used under the chime. Do not dig a ditch under the chime as it may allow settling of a part of the tank bottom and cause leaks.
(d)	Staves.
1.	Place a gasket on the tank-bottom chime in the already described manner. Use punched gaskets, overlapped at gasket joints, and molded chime lap gasket smooth side up under this chime gasket at each joint in the bottom (fig. 76). Drive a drift pin to fair up each bottom lap hole (fig. 77). Determine where stave sheets will fit onto the chime and leave out each stave sheet end bolt. This is done so that a pin may be inserted to line up the staves.
2.	Scatter the first ring of staves in an orderly fashion around the outside of the bottom section leaving about 4-foot clearance between the staves and the bottom. The staves should be concave side up (outside of tank down), with the chime crimp to the left. The drawing which accompanies each tank should be consulted to determine what prepunched connections there are in the staves so that they may be properly oriented.
3.	Successively, block up the right edge of each stave, lay the bolt head retaining channel back side down over the holes, and push bolts down through the channel, the stave and the prepunched gasket. Be sure that the gasket extends one free hole beyond the stave at both ends. On staves that have two rows of bolts, use separate gaskets on each row. Bolts should be left out of the fourth
hole from each end and out of about three other holes so that these holes can be used for pinning. Catch nuts are not needed to hold gaskets and head channel in place.
4.	Place gaskets and bolt-head channels on both edges of the starting stave (fig. 78). The starting stave is the only one which does not have a crimp on either edge. The starting stave is located adjacent to, and to the right of, the cleanout stave. There is no starting stave on either the second or third ring, and on some tanks there is no starting stave on the first ring. A gasket is placed on the right-hand side of all of the staves in these two rings, without exception.
5.	In setting up the starting stave, care should be taken to place it so that its joints will not coincide with the bottom-section joints. Put nuts on all of the chime bolts with the exception of the end ones. Dip a small strand of asbestos in bolt seal and fit it beneath the vertical stave gasket in the crotch where the stave flanges out to form the chime (fig. 79). Place a similar strand under each vertical seam gasket.
6.	Place a chime-lap gasket with its smooth side up, under the right-hand chime end of the starting stave (fig. 80), and each successive stave as it is erected. Raise the second stave, leaving a man to steady the starting one (fig. 81). Slip the lower, left-hand, crimped end in place first. Run a pin through the lap hole to center the second stave (fig. 82), place a bolt in the first hole to the right of the lap hole, and put a nut on it. Work around to the right placing nuts on the chime bolts. Next, insert a pin in one of the vertical holes and press downward on the handle end of the pin (fig. 83). This will pull the channel iron up against the inside of the tank. A bolt next to the pin should then be pushed through from the inside of the tank and a nut made up on it. This process should be repeated at intervals up and down the vertical seam, wherever a bolt hole was left vacant. The remainder of the bolts should then be pushed home from the inside of the tank and nuts placed upon them and tightened. In order tc be sure that all of the boltheads are fitted snugly in the channel iron (fig. 84), tap each one with a hammer. The remaining staves of the ring are erected in a similar manner. Steady the stave until three or four have been attached. If there is a strong wind blowing, it may be necessary to brace the staves with guys to stakes in the ground.
7.	Before the last stave of the first ring is erected
72
Figure 74.
Figure 75.
Figure 76.
Figure 77.
73
Figure 78.
DOUBLE ROW VERTICAL SEAM
CHIME LAP GASKE UNDER STAVE
74
Figure 79.
Figure 80.
Figure 81.
I BOLT HEAD j CHANNEL
| CROTCH))
3.	&
"I c_______
CHIME LAP GASKET
FIRST STAVE
SECOND STAVE
the center pole and rafters should be taken inside the tank. The last or finishing stave of the first ring has both edges crimped and a prepunched clean-out connection. Do not place the cover on the clean-out connection; it should be left clear as an access to the tank during construction.
8.	Tighten the chime bolts, using the extension, socket, speed wrench on the nuts and an open-end wrench on the boltheads. Be sure that all chime bolts are tight, but not so tight that the gasket is crushed. Then, take two ballpeen hammers; hold one underneath the chime and pound the chime lap down with the other, being sure to strike between the bolts. Check the chime bolts again to be sure they are properly tightened. Remove all of the blocks from under the edge of the bottom.
9.	Second and third ring staves are erected with the aid of brackets (fig. 85). These brackets are furnished with all tanks which are more than one stave high, and in the following tabulated quantities:
Number of
Capacity of tank barrels	erection brackets
1,000____________________________________ 14
5,000____________________________________ 26
10,000____________________________________ 37
Erection brackets should be hung near the top of every second stave, around the tank. Fasten the top of the bracket on the third and fourth bolts from the top of the stave and the bottom where it will keep the bracket level. Lay one good quality, 2-inch by 12-inch by 14-foot or 16-foot board between each successive pair of brackets.
10.	Fair up the chime lap holes on the top of the first ring of staves (fig. 86) and place a punched gasket on the chime and molded lap gaskets at each stave joint, just as was done on the bottom chime.
11.	Scatter the staves for the second ring and affix gaskets and bolt-head channels to the righthand side of each one. There are no starting or closing staves on either the second or third tank rings. Lean the staves up against the tank so that they can be lifted up inside of the scaffold and set in place (fig. 87).
12.	Install the second ring staves in the same way the first ring ones were installed (fig. 88). To place the last stave, free the left-hand end of the lower chime of the first stave placed, wedge the first stave chime joint open with a nut, and slip the lower right-hand end of the
last stave chime into this “chime gap” from the inside of the tank. Remove the wedging nut and insert one or two bolts in the chime. Fasten up the right-hand edge of the last stave before fastening the left-hand edge. Be prepared to guy the second ring staves during erection, for strong winds may require it.
13.	The vertical seam bolts of the first ring staves can be tightened during the erection of the second ring. Because of the hazards of falling objects, the men tightening the first ring bolts should npt work directly under those erecting the second ring.
14.	Third ring staves should be erected in a similar manner. Ropes can be used to lift the staves (fig. 89.) Always guy the staves against the wind. 15. In order to get at the inside vertical seams of the second and third rings a “flying cage” of metal or wood (fig. 90), a scaffold, or a ladder must be used.
(e)	Gin pole and rafters.
1.	Slip bottom telescoping extension inside the gin pole, slide this bottom end over against the shell of the tank and pull on the top of the pole with ropes until it is in a vertical position (fig. 91). Loosely fasten two rafters to the gin pole cap (fig. 92) and skid the pole over to the center of the tank, using planks for a skidway (fig. 93).
2.	The outer end of each rafter has a bent gusset which fits between the bolthead retaining channel and the stave, and is affixed with the two top bolts. Where there are two rows of bolts the lefthand one should be used (fig. 94). Inner ends of rafters lap over and bolt to the cap of the gin pole. Adjust the pole as necessary by raising or lowering it on its telescoping foot piece, to fit last few rafters.
3.	Bolt in the short, cross, jack rafters which span from one main rafter to another (fig. 95).
(f)	Roof or deck.
1.	The top chime should be prepared for the deck just as the lower chimes were for the stave rings.
2.	Tank decks are composed of pie-shaf d segments and a center plate similar to those of the bottom and should be similarly assembled. In assembling the deck see that the outer segments fit in under the inner segments, in the manner of roof shingles, to provide water drainage. Place gaskets and bolthead retaining channels on both sides of the starting segment, using catch bolts. This may be done on the ground on one side of the tank from where the segments can be raised with a rope to the tank top (fig. 96).
3.	Outlet connections on the deck should be located and oriented before assembling the deck.
75
Figure 82.
Figure 83.
Figure 84.
Figure 85.
82
76
I SECOND
I StAVE
STAVE TO THE RIGHT
—__——
I FIRST I
STAVE I
FIRST STAVE
I secondI
STAVE I
FIRST VERTICAL . SEAM
BOLT HEAD I
CHANNEL |
•X. „\ope	Sod, etc., replaced
PUMP UNIT1 F / Ip' SAND	EM'
TRAP	o ■^;*^W**
d/Ox>o y •«.	’/■ A	M-	RAMP	„\o<
«(©) BASE	I
xVr	---4--1	X(8JF
**•> /-•....-kF
DITCHPiPE
Figure 101. Suggested layout of a pump station for both camouflage and protection from direct enemy fire.
82
.1,1 1 I
Joping Fill —Covered with Sod, etc. a|	.
^^^^^Drainoge Ditch^Mtajklji^^^^ " I...........SAND O TRAP '
Flow
PERSPECTIVE VIEW
f MAIN LINE
SECTION
ENTRANCE
PUMP UNIT
CAMOUFLAGE
appropriately garnished in desert colors over the tanks. Place similar type fly-tops over the pumping equipment (figs. 99 and 100). Reestablish the natural appearance of the surrounding terrain where flat- or fly-top construction is used.
(6)	Paint tanks and other installations, using a single tone-down or graduated tone-down colors, with appropriate ground painting to assist in disrupting cast shadows.
b.	Prior to starting construction have aerial photographs taken at 5,000 and 10,000 feet elevation. Obtain similar photographs during the camouflage construction work and at the conclu
sion of the work, so that a final check-up and adjustment of camouflage effects can be made.
c.	With respect to concealment of pipe lines in wooded or partially wooded areas, reference should be made to figures 37 and 38.
d.	In figure 101 there is shown a suggested layout of a pump station both camouflaged and protected from direct enemy fire. The station is installed in a pit and concealed by branches, canvas, netting, or other suitable material. This installation must have adequate ventilation at all times, as the tendency for gasoline vapors to settle in low places creates a serious hazard from the standpoint of fire and asphyxiation.
83
CHAPTER 5
OPERATION
20.	TESTING OF PIPE LINE.
a.	As each section of pipe line from one station to another is complete, including the pumping unit, it should be tested, unless specifically instructed otherwise. Pump the line full of water, raise the pressure to 650 pounds per square inch and close the line. Any drop in pressure will indicate leaks. If leaks are indicated, inspect the line, marking all leaky couplings, valves, and joints. Then drain the line; repair or replace al1 defective parts. If the pipe line is to carry gasoline or other petroleum fuel, care must be taken to drain it completely. Drain valves should be placed at the bottom of each dip or valley to facilitate clearing the water from the line.
b.	If the line is being laid in an active theater of operations, there will probably not be time available for testing. In this event serious leaks will have to be repaired without joints. Use stirrup or split repair case of leaky joints; use Dresser leak clamps on leaky couplings.
21.	STARTING THE RECIPROCATING PUMP.
	| •»
5 x<2
NUT
PACKING
SEAT RING
YOKE
TRAVEL PLATE UPPER HALF STEM ADJUSTING SCREW
FOLLOWER
SPRING UPPER
SEAT
PLUG COMPOSITION DISK
BACK-UP PLATE
i	
I is	
	
	
1 1	vsb 1 -	
	i _
	
UPPER
PLUG GUIDE
LOWER HALF STEM
BOTTOM PLATE
DIAPHRAGM PLATE
DIAPHRAGM UPPER DIAPHRAGM CASING UPPER GUIDE ASSEMBLY PACKING LOWER DIAPHRAGM CASING
GREASE CARTRIDGE
CAP SCREW
HW- 1651
13 THD. HEX. NUT
13 THD. HEX. NUT
H W-I37-A
Figure 105. Section and parts list of high discharge relief (Hanlon-Waters type 1626-A).
95
2" HIGH SUCTION RELIEF
PARTS LIST
HW-4 3 04
HW-4303
CAP SCREW
A-862
H W-4 3 0 2
HW-4305
HW-2882
HW-3697
HW-I42-B
HWH744
HW-376 7
HW-3823
HW-2 33 2
HW-2333
H W-4 3 I 8
HW-I2 2I
HW-I37-A
H W-3 8 0 4
HW-3805
HW-3801
HW-3 80 2
HW-3803
HW-3913
HW-3769
		
		
		
		
	k	
	7.	
		
j * 13 THD. HEX. NUT
	
	
HW-I37-A	BODY GASKET
HW-I42-B	SPRING
HW-574	GASKET
HW-912	STUFFING BOX BODY
HW-I22I	GREASE RING
H W-1520	TRAVEL POINTER
HW-1744	SPRING
HW-2 332	PACKING NUT
HW-2333	PACKING FOLLOWER
HW-2812	UPPER SEAT
HW-2813	LOWER SEAT
HW-2882	YOKE
HW-2888	TRAVEL PLATE
HW-3697	UPPER HALF STEM
HW-376 7	ADJUSTING SCREW
HW-3769	SPRING SEAT
HW-3801	UPPER PLUG GUIDE
HW-3802	UPPER PLUG COMPOSITION DISK
HW-3803	UPPER BACK-UP PLATE
HW-3804	LOWER PLUG GUIDE
HW-3805	LOWER PLUG COMPOSITION DISK
HW-38 23	LOWER HALF STEM
HW-3913	BOTTOM PLATE
HW-4302	DIAPHRAGM PLATE
HW-4303	DIAPHRAGM
HW-4304	UPPER DIAPHRAGM CASING
HW-4305	UPPER GUIDE ASSEMBLY
HW-4318	PACKING
A-457	BODY
A-862	LOWER DIAPHRAGM CASING
HW-2 88 8
-HW-1520
H W-912
GREASE CARTRIDGE
HW-574
CAP SCREW f x |f
f- 13 THD. HE X. NUT
A-4 57
HW-2813
HW-2812
f—13 THD HEX NUT
CAP SCREW fx If
-H W-I37-A
Figure 106. Section and parts list of high suction relief {Hanlon-Waters type 1627-A).
96
inches of well-tamped earth over the damaged bottom and installing a new steel bottom on this tamped earth. In such cases, all outlets and inlets in the bottom ring of the tank must be raised to fit the new bottom,
(b)	If the tank shell or roof is damaged, a patch may be welded over the hole, or a rivet or patch bolt inserted if the hole is small. If a large part of a plate is badly damaged, it will have to be replaced.
(4) Remove water from bottom of gasoline and fuel tank frequently. Water has a higher specific gravity than petroleum fuels and will, therefore, settle to the bottom of the tank and can be drawn off from there. After a tank has been filled, its content should be allowed to settle ias long as possible before being withdrawn. This precaution is taken to allow water to settle. Samples of tank contents must be taken with an oil thief and tested in a centrifuge to determine water content. Thief samples should be taken at various levels within the fluid to determine the gasoline-water contact within the tank. Check level of water every day so that it does not reach the tank discharge. Whenever tanks containing gasoline are found also to contain appreciable quantities of water, this fact should be reported to the company commander.
29.	COMMUNICATIONS. Communication equipment used along the pipe-line system should be maintained by personnel specially trained for this work.
30.	SAFETY PRECAUTIONS.
a.	Each individual who is to work with a pipeline system must have a complete understanding of safe practices for his job. The premises surrounding any installation must be kept clean and free from cans and rubbish.
b.	Safe Handling of Gasoline. Men entrusted with the responsibility of handling gasoline have an important function to perform in furnishing fuel to planes, tanks, trucks, and other gasoline-fueled equipment. Any careless act of any one man may result in the grounding of a whole fighter or bomber command, or the immobilizing of armored ground forces due to insufficient fuel for operations. It is, therefore, important that each man be fully acquainted with the hazards of handling gasoline.
C. Gasoline is both an explosive and a highly combustible material. Its fire hazard, however, can be largely eliminated if proper pre
cautions are taken. A gasoline fire cannot be started unless all three of the following conditions are present:
(1)	Gasoline must be present in vapor form.
(2)	There must be sufficient air present to support combustion.
(3)	The gasoline vapor-air mixture must be ignited by flame, spark, or some other source of sufficiently high temperature.
(4)	Elimination of any of these factors will prevent fire. Thus, if gasoline is stored in closed containers, there is not sufficient air to support combustion. When, however, the gasoline is exposed to the air, sources of ignition should be eliminated.
d.	Fire hazards.
(1)	Spills, leaking joints, leaking hoses, and nozzles are the most common causes of fires, and these leaks should be carefully guarded against. Leaks should be repaired as soon as they are found. Spilled gasoline should be wiped up and the gasoline-soaked rags disposed of at once.
(2)	Gasoline-soaked clothing should be removed as soon as possible and the parts of the body exposed to the gasoline washed thoroughly with soap and water. Wearing clothing soaked with gasoline creates a dangerous fire hazard, and painful blisters may be caused by the gasoline coming in contact with the skin. Burns caused by such direct contact with gasoline should be treated in the same manner as burns caused by fire. Gasoline containing tetraethyl lead is especially dangerous.
(3)	“No Smoking” signs and regulations should be posted in the danger zones and the regulations strictly enforced. Smoking or striking matches near gasoline refueling stations or near breaks in lines or at pump stations must be prohibited.
(4)	Open flames or lights, other than the approved safety type vaporproof lights, should never be permitted on or near storage tanks, tank trucks, loading stations, pump stations, or other areas where there is a possibility of gasoline vapors accumulating. The personnel working in these areas should not carry either matches or lighters. This rule should be rigidly enforced. Always be on the safe side, even though it requires a little more time and effort.
(5)	Do not allow gasoline to remain in open containers, containers should be tightly closed at all times. Do not use gasoline to clean floors, start fires in stoves, or to wash pump engines or other machine parts; use special safety solvent or kerosene.
97
(6)	Hammering or pounding on any line or fitting which contains gasoline under pressure must not be permitted. Caution must be taken to relieve line pressure before breaking into any line, such as by removing a pressure gage or plug. Valves should never be opened or closed unless accurate information has been obtained as to just what purpose they serve. A leaking valve on a high pressure line must never be stopped with a bull plug; a nipple and an extra valve should be used, the second valve being open while making the connection.
e.	Precautions to be taken while repairing leaks on gasoline pipe line.
(1)	Trucks and cars should stay a safe distance from a leak and always approach from the windward side.
(2)	Gasoline vapors are heavier than air; therefore, never approach a leak with a car from a lower level.
(3)	Repair crews must know first aid, and especially how to give artificial respiration and treatment for burns.
(4)	Adequate first aid material, including burn ointment and blankets, should always be available.
(5)	Only nonsparking tools (hardened beryllium copper) should be used in repairing leaks.
(6)	Goggles should be worn by men making repairs.
(7)	It is necessary for men to use rubber or Duprene leakproof boots when standing in gasoline.
(8)	Every precaution possible must be employed to prevent a spark while removing and replacing sections of pipe line.
(9)	Pit holes must not be spot-welded; use clamps. (10) Even after a leak has been repaired, continued care must be taken to prevent a flash and fire. Two or three days may be necessary to make the vicinity gas free. Test should be made with an approved gas indicator.
f.	Static Electricity.
(1)	A combustible mixture of gasoline and air may be ignited by an electric spark resulting from static electricity. A static-electrical discharge is caused by a difference in static-electrical potential between two objects. An example of one way in which static-electrical potential may be built up is by the friction which develops when walking with leather-soled shoes across a carpet. If, under conditions just described, the person reaches out to touch a metallic object which is at a lower potential, such as a door knob, a spark will jump just before the metallic object is touched. Simi
larly, a static-electrical potential is built up on a gasoline-tank truck as the truck moves along a road. The accumulation of a static charge on any object and sparks resulting therefrom can be prevented by keeping that object at ground potential.
(2)	In the case of gasoline trucks the following precautions should be observed:
(a)	Ground the truck to the loading-rack piping before the fill-cap is removed from the truck. The truck should be grounded as long as the tank is being filled because a considerable static charge is generated by the flow of the gasoline through hose, nozzle, and air while flowing into the tank.
(6)	Each tank truck should be provided with a drag chain connected to the truck chassis, axles, and tank itself, to maintain all parts of the truck at the ground potential.
(3)	Railroad rails frequently carry an electrical current, and where this occurs, care should be taken to prevent a spark at any point where cars are unloaded. This is usually done by insulating the loading rack section of the tracks from the spur or main line, grounding this section by bonding the rails together with copper cable, and connecting the cable to the same ground connection as the car unloading piping. This brings the car to the same potential as the piping and unloading equipment and keeps it that way during unloading operations.
(4)	Above-ground piping and tanks should always be grounded. If the tanks and piping are underground, no further precaution is necessary.
g.	Demolition. All operating personnel of a pipe-line system should be instructed in the proper methods of demolishing the system, in case it becomes necessary to prevent it from falling into enemy hands. The completeness with which any pipe-line demolition program can be carried out depends upon the time available. A simple and effective method of demolishing a system which is being used to transport gasoline is to break the fuel line to the gasoline engine which powers the pumping unit and set the pump station on fire. Setting fire to gasoline in tanks will destroy them effectively. Where water is being handled the tanks should be filled and then destroyed by charges of explosives. Explosives may also be used to quickly and efficiently demolish pump stations. The demolition of the pipe line presents a more difficult problem. Where time is available, the line can be rendered unserviceab1e by smashing the cou-
98
SCHEMATIC SKETCH OF PROPOSED PLAN FOR GASOLINE TRANSPORTATION & DISTRIBUTION IN THEATRE OF OPERATIONS / . . . 1st PHASE
I
j-*—PIPE LINE
LOADING DEPOT
WATER
BEACHED LIGHTERS
RESPONSIBILITY OF____,
SHORE AMPHIBIOUS GROUPS
FLOATED CONTAINERS
FILLED CAN DUMP
FREIGHTER
Figure 107. Schematic sketch illustrating initial phase of gasoline transportation and distribution.
j
/
99
FILLED CAN DUMP
ARMORED
DIVISION —
DUMP
AIR FIELD DUMP
EMPTY CANS
SCHEMATIC SKETCH OF PROPOSED PLAN FOR
GASOLINE TRANSPORTATION & DISTRIBUTION
IN THEATRE OF OPERATIONS . ... 2nd PHASE
k- PIPE LINE
TANKER
FREIGHTER
WATER
MARINE LINE
BEACHED LIGHTERS
DOCK
RUM
CORPS OF
ENGINEERS
EMPTY CANS
ENGINEERS
Q. M. C.
XXX
TANK
FARM
LOADING DEPOT
AIR FIELD j DUMP
FLOATED
CONTAINERS -
FILLED CAN DUMP
FILLED CAN DUMP
FILLED CAN DUMP
DISPENSING UNIT
FILLED CAN DUMP FILLED CANS
RESPONSIBILITY OF SHORE AMPHIBIOUS
GROUP ri(irrxw_ FIL L E DJia CAN DUMP
H
ARMORED DIV. DUMP
air'field
DUMP
BOOSTER MATERIALS & EQUIPMENT FOR PIPE LINE BATTALION HANDLED BY AMPHIBIOUS GROUP
Figure 108. Schematic sketch illustrating second phase of gasoline transportation and distribution.
100
Q. M. C
filled cans! V
EMPTY CANS __
TANKER
FREIGHTER
BEACHED LIGHTERS-^
I DOCK
■*
CORPS OF
ENGINEERS
*
PIPE LINE
EMPTY CANS
TERMINAL TANKS
TERMINAL TANKS
Q. M. C.
FUTURE PIPE LINE EXTENSION}
Figure 109. Schematic sketch illustrating third phase oj gasoline transportation and distribution.
IN THEATRE OF OPERATIONS . ... 3rd PHASE
ARMORED DIV. DUMP
FUTURE PUMP-*
MARINE
‘ LINE
FLOATED
CONTAINERS
PUMP STATIONS
AIR FIELD DUMP
PUMP STATIONS
FILLED CAbfS
FILLED
CAN DUMP
RESPONSIBILITY OF SHORE AMPHIBIOUS GROUP
FILLED CAN DUMP
DISPENSING UNIT
FILLED -CAN DUMP
FILLED CAN
DUMP
FILLED CAN
AIR FIELD DUMP DUMP
DISPENSING UNIT
________r*--. PIPE LINE | LOADING DEPOT |
SCHEMATIC SKETCH OF PROPOSED PLAN FOR
GASOLINE TRANSPORTATION & DISTRIBUTION
-
Xj|t. VALVE DISPENSING
UNIT
ENGINEERS
BOOSTER PUMP ||Z MATERIALS & EQUIPMENT FOR PIPE LINE BATTALION HANDLED BY AMPHIBIOUS
II GROUP
TANK
FARM
101
Q. M. C
FILLED CANS EMPTY CANS I---->---------
plings with sledge hammers and flattening the pipe. The important part to be destroyed is the pump station equipment, particularly the engines and pumps. There will be assurance that serviceable pumps and engines cannot be assembled from damaged ones if identical parts, such as pump casings and engine distributors and carburetors are destroyed on all units.
31. PHASES OF FUEL SUPPLY. In any operation involving the establishment of a beach head or landing point the supply of fuels will be handled in three phases, as follows:
O. Figure 107 illustrates the initial phase in which fuel required is transported to the beach head in freighters and lighters, or floated ashore in metal cans or containers where it is stored in dumps. From these dumps or storage points the containers are moved forward by the Quarter
master Corps to points of use. Empty cans are;’, returned to beach head for refilling.
b. Figure 108 illustrates the second phase of | operations in which the Corps of Engineers hasi made its initial installation for the bulk storage of fuel in tanks, augmenting that stored by the Quartermaster Corps in cans. The Engineer I function is to install and operate a marine line from tanker to tank farm and to distribute to the Quartermaster Corps dump through pipe lines, jl^
c. Figure 109 illustrates the third phase of the operations in which the Corps of Engineers has extended its facilities to serve the various dumps established by the Quartermaster Corps during the first and second phases. This has been accomplished by the installation of pipe lines, stations, and terminal-storage tanks. Provisions are made for future expansion to forward areas as required.
102
CHAPTER 6
AUTOMATIC AND MANUAL CONTROL
32. AUTOMATIC CONTROL FOR RECIPROCATING PUMPS. This type of pump is controlled by a hydraulically operated diaphragm throttle connected directly to the carburetor of the gasoline engine used to drive the main line pump. Figure 110 illustrates the hydraulic engine control system. The complete control system, including relief valves, is shown in figure 112. Pressure in the hydraulic engine control system is maintained by the small rotary oil pump (OP) which circulates a mixture of kerosene and motor oil through the system. Any increase in pressure in this system brought about by restricting the flow of the control fluid is reflected directly on the head of the diaphragm throttle (DT), which in turn moves the carburetor arm toward a closed position and reduces the engine speed. A drop in pressure in this system caused by decreasing or removing the restriction to flow of the control fluid lowers the pressure on the diaphragm throttle and allows the spring in the throttle head to move the carburetor arm toward the open throttle position and increase the engine speed.
a.	Control Oil Pump. The control oil pump is a small, rotary, positive-displacement type pump, chain-driven from the magneto shaft of the engine. Under normal operating temperatures, the control system fluid is made up of a mixture of 70 percent kerosene and 30 percent SAE 10 motor oil. In hot climates the mixture should be 50 percent kerosene and 50 percent SAE 10 motor oil. In extremely cold climates this mixture should be 90 percent kerosene and 10 percent SAE 10 motor oil. These mixtures have sufficient
lubricating characteristics to prevent excessive wear in the control oil pump. Do not experiment with other lubricants.
b.	Oil Relief Valve. The control system is protected against excessive pressure by a diaphragm-actuated, spring-loaded relief value (RV), shown in figure 110, which can be adjusted to open
and relieve at a predetermined pressure. Excessive pressure in the control system will result when any restriction approaches or becomes a complete closure against the discharge of the control oil pump. Control oil pressure acts continuously against the diaphragm of the oil relief valve, and when the predetermined relieving pressure is reached this relief valve will open immediately and allow the control oil to flow directly to the oil reservoir (OR). When the pressure falls due to the reduction or complete removal of the restriction in the control oil system, the relief valve will close and normal oil circulation through the system will be resumed.
c.	Orifice Valve. The orifice valve is a standard type of hand-operated needle valve placed in the system for use in adjusting the automatic controllers and relief valves. It may also be used in changing over from automatic to manual control and as a means of limiting the maximum engine speed.
d.	Low Suction Controller.
(1) The low suction controller (LSC) regulates the engine speed so that the pumping unit will, within certain limits, handle all the liquid delivered to the suction side of the pump and at the same time maintain a constant predetermined minimum suction pressure. The low suction controller is of the spring-loaded, diaphragm-actuated type and is installed in the control oil system as shown in figure 110.
(2) The diaphragm space in the head of the low suction controller is connected to the pump suction by a small copper tubing. A pressure snubber (SPS) is installed in this line to reduce the transmission of suction pressure impulses to the controller diaphragm. By means of a spring adjusting screw, the controller spring is set to cause an upward force on the lower side of the diaphragm. In a state of equilibrium, this spring force must balance the force exerted by the suction pressure
103
GP
DIAPHRAGM
VALVE
THROTTLE STOP NUT
T SN
OCK NUT

CLOSED
SUCTION
rrrmwit
BOTTOM
DISCHARGE
FLOW
Figure 110. Hydraulic engine control system.
HYDRAULIC ENGINE CONTROL SYSTEM
UPPER 'STEM
LOWER STEM
UPPER STEM
SPRING ADJ SCREW
LOWER STEM
LOCK NUT
LOWER STEM
LOCK NUT
MANUALLY OPERATED
SEAT RING HW- 3868-
CONNECTION TO CARBURETOR
j COPPER
\ TUBING
CLOSE TIGHTLY WHEN MANUALLY CONTROLLED
RANGE IO*TO 50
j COPPER TUBING
INNER VALVE HW- 3786
SUCTION PRESSURE SNUBBER
S PS
-HW- 4286
INNER VALV
SEAT RING
HW- 3868
OIL PUMP
OP
ENGINE ' E
HIGH SUCTION CONTROLLER
HSC AUXILIARY GOVERNOR PRESSURE
AGP
LOW SUCTION CONTROLLER
L S C
CONTROL OIL RESERVOIR OR
MADE HERE FORI MAX. PRESSURE
STRAINER s
RELIEF VALVE
R V
RANGE 300* TO 650
DIAPHRAGM
SYNCHROSTART ‘"'OSG“
SPRING — ADJ.
SCREW
ORIFICE
O V
differential
PRESSURE
CONTROLLER
DPC |
DIAPHRAGM THROTTLE
DT
104
DISCHARGE n PRESSURE HU DPS
S-P range 50* TO 350*
1ARGE SURE
DETAIL OF CONTROL PILOTS
riN.P.T. i CAP SCREW.	PARTS LIST
\	1/5 STD. NUT
HW 3931 x	\	/
I lit ,o.
HW 3891—V XTZZTTf l -T I ill ILhW 4130	HW 70-M PACKING
T ZZ Z/Z/iX- S I I I MJU —nw*nou	HW 130-A SPRING
HW393O^	I i -J—-TT1 ■ I.ll	HW 132-C SNAP RING
HW3R9iT^£=S?5WrEi r^^iT7rn	HW 203 spring
nwjayi FFF/I	I II' fronv	HW 574 STUFFING BOX GASKET
lll /l^T...	HW 862 UPPER DIAPHRAGM CASING
HW3894—.	'll I I THt/ CARTRIDGE ,	*	HW 894-B SPRING
HW 574	ItfHrrZ I » ml I □ X	In.P.T-x	,-p ^crfw	r4*NPT	HW9I2 STUFFING BOX BODY
HW9I2------tJJflJ^lST.-ELL HW352z/\	/2 CAP SCREW	r< r'HW_3527 HW 1221 GREASE RING
HW 1221____It- i KJ	X V-!r	rr—n	I \	rZ-n	rrtl	\	/ r-r-ri HW 1442 DIAPHRAGM PLATE
HW2937_____F / ~~K ? nr 1 IT HW 862^ ;l	IM |'|hW862^. 'I	FLi I HW 1682 UPPER SPRING SEAT
r T I	I/HW3895 T ZxZ/Z/Z/I T I I 11	’ ZZ/wZXX"' /	|^	[l'| HWI685 LOWER SPRING SEAT
HW2333-----_l! H rp ' I’ Tl HWICag-p- 1/ JX-Th	I I JHWI688. £ -	__/ I | | , || HW 1686 STEM GUIDE SLEEVE
HW2332—----.L-qMsdJb Ur HWI768-----------™*l*"g™*l*™,!:S3~|HW'l44P TP	" ‘"ll ..I"" I l'';i HW 1688 LOWER DIAPHRAGM CASING L.P.
HW4I29---I	11 । HWI686 F=\rTTTTj	IH W1686 ~ N s	I	hl H W 1688-B LOWER DIAPHRAGM CASING HP
HW4I70_____	|lI I HW 1739 —-,	1______ |JhWI739	| | .J H W 1725 YOKE COVER PLATE
HW 3884	Z4"~	HW [32°c2j|	1 ' T^^NhW ItS^V	1 I 11 ‘ill ” RETAINING^WASHER
j*STD nut-^TT ^J1	J lW yKW9 / [W K.l?
Uin mi it__________W	r TX	II	5 CAP SCREW//	|	HW 2332 PACKING NUT
i4 STD. NUT	| «L h HW894 B FlSX	HWI682--I	HW 2333 PACKING FOLLOWER
2	3.	i	A629 ————^7	II	HWI30-A - /// SS"	I	HW 2755 BODY GASKET
HW 203  -------4 |	j	S—-	\	A629   */	|:<	HW 2920 BONNET
A	f a,	\	Z	\	/ 7 I	\ HW 2923 PACKING FOLLOWER
A629 -------7L*Z SC	/fe 4 "XS	Z\	L^7	।	HW 2937 PACKING
/7~V f. rpxZt	rv\	r\ f SSkB I	r\ f ^xz.'	r\ HW* 3527 diaphragm
HW 1685 ———7 O	O\ HWI685 ——Z-Q-	:	O\ HWI685 ZO	O\ H W 3786 IV. LOW SUCTION
/	_ 4 J |	1	/zz T	JS“-|	/ A T I ______________| H W 3824 UPPER STEM
HW I725 ——J^7 7777777 ।—L-L-U-L ==J HWI725--4-TZ^Z/Zt-----/.Il	HWI725--L	.	| ll	HW 3868 SEAT RING
T 7E//7777 k ' — /	\	7/////Y / j I — I	27////A l»| I / HW 3884 UPPER SPRING SEAT
HW 4075----W4 -----X X | O / HW4075---------ZfT ----4, X D/ HW4075-----------\-f=y ---Ti \ (~\ I HW 3891 DIAPHRAGM PLATE
\W- g \i \^/	\V r V I	s il HW 3894 distance piece
HW 3896 X J Xi / HW3824-— V T	it X HW 3824 X T	HW 3895 UPPER STEM
HW 3896 —. F /	HW3»44—-----\	i	y HW3824—Z ;	/ HW 3896 STEM SUB.
‘--	T>----IO-32xi	x . .....I z >--------IO-32xg	"---\A HW 3930 LOWER DIAPHRAGM CASING
jS.AE. NUT--------- X	|!Z RD. HEAD	—-•HI.	1/ Rp. HEAD	___HW 393I UPPER DIAPHRAGM.CASING
x ■	A\\	£s.A.E. NUT—-'	|	7 1S.A.E NUT— ’ 7]	HW 4075 ADJUSTING SCREW
HW2923—------~	/ III HW2923______-____\	/' i	HW2923------ (	HW 4130 DIAPHRAGM
’CAPSCREW_____Z II	iCAP SCREW--— zfc^r / I I IcaP SCREW-----------HW 4170 HOLD DOWN RING
gCAHSCKLW	y \ H______-HW2755	xUTT y y------------HW2755	HW 4286 INNER VALVE
HW9O,n_________uxJ-PT . ‘	kxlri T IJl	i—1 Hl	i a 629 yoke
HW2920	~RSnl "'Zi ill _^-HW4286	—X—..< ■ ;l	HW 2920 ----^706$ , I ' II]	A 806 BODY
HW70-M---------HW 2920—2/L------------------------I	HW 70-M-------
Tnpt—	hw70-M—//I g^s^i 11Wp	.	I'—®
_I—__wW — | HW 428er	T_i~r~~------* N-P,T—~~~ri MT	~ ~~L—Jn.pt.
HW 3868--------/TXT yy~)	HW3868—-------HW 3868------------------------ pT/Z^Vl — —i|
. RnR ________|	।	HW3786-------—/
-------------A806 ----------------------------MpUI A806 ------------------------/L j( TZ_-----------------------fN.P.T.--------------Z_.------------ I'n.P.T ---------—T
DIFFERENTIAL PRESSURE	HIGH SUCTION	LOW SUCTION
CONTROLLER	CONTROLLER	CONTROLLER	,____________________________
WOW..HC W«—U««-_IM mvi.>O-»	F.TTXMM
222________T,T" CONTROL PILOTS "tv~I625
owh c««	HANLON-WATVIt*, IMC. «»Q o . -
'	■ ■	____________________________________________________________________________ »cxv« V4 « I OAt. 8-IOMq	TOUAOKLA._ 0^48
Figure 111. Details of control pilot.
105
BV-2	CV	BV-I
DOWNSTREAM	I	/I
,-----------------------------	PxXkHWeLM er-^^w uwncy
I	I I	I I	I 4’ PIPE
----1--1 DISCHARGE VALVE	\y	\1 \y	I Lx^ \ / Dv	V/
\	/	NORMAL FLOW	\	/
\/ X.......................	.... u	SUCTION \ /
Y	DISCHARGE HEADER	4 PIPE	A	VALVE V
A	d*	5V A
/ \	LT'2,~\ (--------■> । / \
el	z—rA
r fiw S6	*	X^X
WjT rj$K	DISCHARGE CONTROL LINE	>	/ X
Uli ill __________________________2£k_._,____________________	/_________J
LT-|7___|3I E*h	Lu 17—\ Lu'14-\ *rLU-'3’	r-i-u-32 yiu'? rLU'3
I cs Pa	\	\ \	1_______■0'iiM	sand
'AbH ify	\	✓V~\—~~~ I -rn-CA > B 1 jfl	trap
I8	st
|| i| s! „	> «?■ sSk *9 Lu 21—wEUWnEnWrWl	tTflr^zPM si ; K
gt g	/w	inWlTl xv- /	o
3 ° LT‘ m------tT—n	A V	\y——I——J	LUfli J BUJ
u' “■	In -f	~	LOWER STEM /X— I —/---^y U । / g 	>-—-
< LT- 31-------1---3if-Cf| I	AUVSTNG NUT locx nutToRJ ~LX^ir^ HHLJlBBI
1 Si	[	I I	LOWER STEM *~UH0
I 11 LOWERStST/----wF H I I 5	HIGH DISCHARGE RELIEF	---<^SnX^
LT- 32-1---J| I J	H D R	/
LT-I® P- - -flfjfc | E .	*	.
liU	1
kWfl'RUSU	»
WlE#7	i	K
LMO	^header	f
lT-4___	BY-PASS FLOW	SJH	°	~
lt- 2 —-	Hl | 1)/^	~ ~	'	~	\. y
LT’ 3 N	SUCTION	J ____ ______L„_
Jl-Mh	SNuSf^fl^	'p^pJlSCHARGE 1
s PnSJ H '	/
HIGH SUCTION RELIEF	MB it	I I	'4
HSR	U ’as’ I 4BJME----' '---pump.-x
SUCTION I J___ SUCTIONII ■
fps -[■'-■■ PS 1 /%	C-4_____________________j
i	tcXll I IVkZzI	' m DISCHARGE | 
V.	’ n	PRESSURE |
k»	SNUBBER I
Tgp	ysp AA^fDP	; FW dps ;
.•	z---------X	50* TO MO______________ J____J_________J	|.
vi COPPER r	1--------------
\TU8ING |_____ J
HANGE , (	TrANGE	'	i
» T° 50	/-OIAPHRAGM'^	300* TO 050* /TunS	*	J	!	’ 1-------1
rm OIAPIRAGM7 MjUa ff k"U----
TnH R iT	------------------<	।
UPPER _[ QD I H I	"*	]|	I
STEM tfjcdfeiijU	'	•;
f	I life I _.»««_L-llI	S	!	h
/I iHv~^T“ /Fli \	lower—/IJi \
/° Mlpa oy 5T“ 7otzlfcJo\	:	!	'
«u~- V. Ca^X^	I HA	5”""°	pump	I I
saew A« 0/	TJZ 0/----s&r-ip	I	p
Y-IOBB s™---,T.	„„ AP X-UM> Situ	I	|l
' l-JfT UKS WT	T- JFl — IHMSR VALVE- 10 T	LOCK MIT
SEAT RIW W IfaL - {COPPTA	ifafel »AT RIH® LgflLJ	>	l|
w	\tubinc	. -nw-3«« tg||ga	G
B*	A	MAMUUV
LOW SUCTION gm HIGH SUCTION_ /operated CONTROLLER	CONTROLLER	< L» - I close tightly J—-------------1	I
, Tl!:	i-iccr 1«	differential fc S53B4 wher manually	L-belt
LS C ------s.	AUx»iarv	kk	PRESSURE	W** I B-HKOU-EO	|	1^^ I
> aWEJBNOR	F*3	CONTROLLER ORIFICE VALVE	1	|! V B D !
o pb«sure	D p c	O V	-------------------------- I
pr^ *yx AGP v	j
3 J , , ADJUSTMENT-1	-_________'_______________s.______________________
r '	I	I	A THROTTLE STOP NUT	I
It	TSN kj i ;
® 8	__________ ___^zz?....	1 <	----=7,	C0NKCTI0H TO J I	t
L	1 j W v.ir"",",ie