US3158193A - Fuel supply system - Google Patents

Fuel supply system Download PDF

Info

Publication number
US3158193A
US3158193A US12404761A US3158193A US 3158193 A US3158193 A US 3158193A US 12404761 A US12404761 A US 12404761A US 3158193 A US3158193 A US 3158193A
Authority
US
United States
Prior art keywords
valve
tank
fuel
tanks
valve seat
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
Inventor
Glenn R Anderson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mcculloch Corp
MC CULLOCH CORP
Original Assignee
MC CULLOCH CORP
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MC CULLOCH CORP filed Critical MC CULLOCH CORP
Priority to US12404761 priority Critical patent/US3158193A/en
Application granted granted Critical
Publication of US3158193A publication Critical patent/US3158193A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/02Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
    • B63B1/04Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/0047Layout or arrangement of systems for feeding fuel
    • F02M37/007Layout or arrangement of systems for feeding fuel characterised by its use in vehicles, in stationary plants or in small engines, e.g. hand held tools
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/0076Details of the fuel feeding system related to the fuel tank
    • F02M37/0088Multiple separate fuel tanks or tanks being at least partially partitioned
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2559Self-controlled branched flow systems
    • Y10T137/2564Plural inflows
    • Y10T137/2567Alternate or successive inflows
    • Y10T137/2569Control by depletion of source
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/4673Plural tanks or compartments with parallel flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7287Liquid level responsive or maintaining systems
    • Y10T137/7358By float controlled valve
    • Y10T137/7365Single float controls plural valves

Definitions

  • This invention relates to fuel supply systems and storage tanks-and more particularly to apparatus enabling fuel to be withdrawn from a plurality of tanks one at a time.
  • While the invention is suitable for a variety of applications, it is particularly well sui-ted for use in supplying fuel to the motor of a motor boat or the like.
  • Many small boats, such as runab-outs, and the other outboard motor boats do not have enough available space for a single large fuel tank.
  • the small boat operator who cannot employ a single relatively large tank, or the boat operator who must carry gasoline to his boat, it is necessary to keep several small fuel tanks in the boat in order yto run the motor for extended periods of time.
  • the tanks In applications such as boating, it is impractical as well as hazardous to pressurize the tanks. Moreover, the tanks must be portable, independently movable, and easily detachable. VThe required valves must be relatively simple in construction and low in cost in order to be of practical value. Moreover, the redirecting or transfer of flow from one tank to the next must be entirely automatic, reliable in operation and must not cause interruption of fuel flow during the transition period. Furthermore, for several reasons it is desirable to empty each of the tanks entirely before -any fuel is Withdrawn from one of the other tanks.
  • t is still another object of this invention to provide an improved fuel transfer system employing a plurality of similar portable interchangeable fuel tanks each including a fuel transfer valve therein and wherein said valve is relatively simple in construction and low-in cost.
  • the present invention provides a fuel tank transfer system including a plurality of separate independently movable or permanently fixed storage tanks.
  • Each of the tanks has .an open fuel inlet connection and an open fuel outlet connection and each tank includes a float operated valve. This valve is preferably contained within the tank.
  • Each of the float operated valves includes a second valve seat communicating between the inlet connection and outlet connection of the tank.
  • a movable valve element provided in the valve includes a second 'valve head adapted to cooperate with the second valve seat.
  • a first valve seat communicates with the outlet connection of the tank and the interior of the tank.
  • a movable valve element including a first valve face is adapted to cooperate with the first valve seat.
  • a float is operatively connected to each movable valve lelement to move the second valve face into contact with the second valve seat when the float is urged upwardly by the fuel in said tank and out of contact with the second valve seat when the float is moved downwardly thereby allowing fluid to flow from the tank inlet connection to lthe tank outlet connection when the level in the fuel falls below the level of the float.
  • a float is operatively connected to the first said movable valve element to move said first valve face onto the said ⁇ rst valve seat when the second valve face is out of Contact with the vsaid second valve seatl and away from Vsaid first valve seat when the second valve face is in tanks is adapted to be connected to an engineV or to other device requiring fuel.
  • each of the tanks includes a valve vcomprising a housing having two inlet openings therein and a single outlet opening.
  • One of these inletopenings communicates with the interior of the tank and the other of y said inlet openings is adapted to be connected to the outlet connection of one of the other of the tanks.
  • the valve comprises a housing having an opening or bore therethrough with' first and second spaced .apartr valve seats therein. Each of these Valve seats is provided with a valve port or opening therein.
  • the bore is divided i bore disposed vertically so that one of the end chambers comprises an upper end chamber and other of the end chambers comprises a lower end chamber, the lower end chamber communicating with the interior of the tank and the upper end chamber communicating with the inlet connection of the tank.
  • the outlet connection of the tank communicates with the central chamber.
  • valve head When a single movable valve element is used, it is preferably slidably mounted within the bore and is provided with a valve head at each end.
  • the valve heads are preferably positioned within said central chamber, in which case, the float can be rigidly connected to the lower end of the movable valve element.
  • the valve heads can be spaced apart and each positioned in one of the end chambers and in this instance the oat is preferably connected to one end of a lever arm, the other end of which is operatively connected to the lower end of the movable valve element.
  • FIG. 1 is a vertical longitudinal sectional view of a boat and motor utilizing the present invention.
  • FIG. 2 is a semi-diagrammatic vertical sectional view of the fuel transfer system according to the present invention.
  • FIG. 3 is a vertical sectional view of a fuel iiow transfer valve of the present invention.
  • FIG. 4 is a vertical sectional view of another form of iiow transfer valve of the present invention.
  • FIG. 1 a boat 10 and motor 12 secured to the transom 14 of the boat 10.
  • Means for transferring or pumping fuel comprises a fuel pump 16 secured to the motor 12.
  • a pump outlet duct 18 is connected between the outlet of pump 16 and the carburetor (not shown) of the motor 12.
  • the inlet of the pump 16 is provided with a quick disconnect coupling 20 of known construction.
  • a yplurality of similar interchangeable portable fuel tanks 22 provide fuel for the engine 12. While any number of such tanks can be used, three such tanks are shown by way of example.
  • Each of the tanks 22 is provided with an open inlet connection 24 and an open outlet connection 26, a removable lill cover 28, a fuel transfer valve 30 within the tank and carrying handle 32 connected to the upper surface of the tank.
  • the inlet connection 24 and outlet connection 26 of each of tanks 22 are preferably provided with quick disconnect couplings 34.
  • a duct or line 36 is secured between the inlet connection 26 of the tank 22 at the left in FIGS. l and 2, and the pump 16.
  • Another fuel duct or line 37 is secured between the inlet connection of the same tank and the outlet connection 26 of the center tank of FIGS. l and 2.
  • a similar fuel line or duct 38 is connected between the inlet connection of the latter tank and the outlet connect-ion of the tank 22 at the right of FIGS. l and 2.
  • the lines 36, 37 and 38 may be easily and quickly disconnected at either end thereof when it is desired to fill the tanks or remove them from the boat.
  • the tanks of course, are lilled through the opening cover by the ll cap 2S.
  • each tank 22 Connected between the inlet connection 24 and the valve 30 of each tank 22 is an inlet duct 42 and connected between the outlet connection 26 and each of valves 30 is an outlet duct 44.
  • the tanks are thus connected together in series, the outlet of one tank, being connected to the inlet of the next adjacent tank and as many tanks as required can be thus connected together in series.f It is understood, however, that the inletv connection of the trank at the end of sucha series of tanks will have no fuel line connected thereto and also. the tank at the opposite end of such a vseries of tanks-will have its outlet connection connected to the inlet. of the enginel 12.
  • Ducts 42 and 44 are preferably metal conduits which in addition to serving as fuel lines are used to position the valve 30 securely within the tank. As shown in FIG. 2, the valve 30 is positioned at the bottom of the tank 22 with the lower end thereof against the lower surface of tank 22.
  • FIGS. 3 and 4 show two valves 30 according to the present invention. These valves'are similar in construction except as described hereinbelow;
  • the valves 30 include a housing 48 which is cylindrical in crosslsection and of somewhat greater height than width.
  • the housing 48 is provided with a vertically extending opening or bore S0 therein which extends from one end to the other.
  • the bore 50 is provided with a reduced diameter to form a irst valve seat 52 and a first valve port 54.
  • the bore 50 is screw threaded at 56 to receive a removable valve seat member 58.
  • Valve seat member 58 includes a second valve port 6G and second valve seat 62.
  • the first and second valve seats 52 and 62 respectively divide the bore 50 into a pair of end chambers 64 and 66 and a central chamber 68 between the valve seats 52 and 62.
  • the valve chamber 64 comprises an upper valve chamber and the valve chamber 66 comprises a lower valve chamber.
  • the upper end of the bore 50 is screw threaded at 70 to receive an adapter '72 to which the inlet duct 42 is secured.
  • the adapter 72 is provided with an opening 74 therein to allow communication between the duct 42 and the upper chamber 64.
  • the housing 48 is bored and threaded at 76 to receive an adapter 78 to which the outlet duct 44 ⁇ is secured.
  • the adapter 78 is provided with an opening 80 to allow communication between the outlet duct 44 and the central chamber 68.
  • valve Sil is provided with a movable valve element 82.
  • the movable valve element may be conystructed in various ways, according to one form of the invention, it comprises a shaft 84 concentrically and slidably mounted within the bore 50 and extending through the ports 60 and 54.
  • Shaft 84 is of a sufliciently y small diameter so that it will not obstruct the flow of fuel through the ports '54. and 60.
  • a valve sealing element 86 preferably formed from resilient material such as rubber.
  • the valve sealing element 86 includes a first valve head 88 at .the lower end thereof and a second valve head 90 at the upper end thereof.
  • Each valve head includes a frustoconical valve face and the valve face of the lower valve head 88 is adapted to cooperate with and seal the first valve seat 52 while the upper valve head 90, and its valve face, are
  • iloat 92 Operatively connected to the movable valve element 82 is a iloat 92.
  • the oat 92 is rigidly secured to the lower end of the shaft 84 and is 4entirely contained within the chamber 66.
  • the float 92 will rise causing the upper valve head 90 and its valve face to seal the valve seat 62 andthus close the port 6B.
  • Shaft' 192 has mounted concentrically thereon at the upper and lower ends thereof a pair of spaced apart valve heads 104 and 166.
  • the valve heads 104 and 105 are secured to the shaft 102 rigidly by any suitable means such as adhesive and they are preferably formed from a resilient material, such as rubber.
  • Each of the valve heads 104 and 1% is spaced outwardly of the valve ports 54 and 6i?, the lower valve head 104i being adapted to cooperates with an seal the valve seat 52 of port 54 and the upper valve 106 1oeing adapted to cooperate with and seal the port e0 of valve seat 52.
  • Each of the valve heads 104 and 106 are provided with tapered or frustoconical valve faces adapted to seat against the respective valve seats.
  • lever arm 110 Pivotally connected to the lower end of the housing 4S by means of a horizontal pivot pin 108 is a lever arm 110. Connected to the outward end of lever arm 110 is a iioat 112. The opposite end of lever arm 110 is operatively connected by any suitable means to the lower end of the movable valve element 100. For purposes of example, this connection is shown as a il-shaped fork 113 including a pair of prongs which extend on either side of the shaft 102. A pair of spaced apart stops 116 and 11S are provided on shaft 102 to limit the upward and downward movement of the fork 113 thereon.
  • chamber 66 In the valves of both FTGS. 3 and 4, the lower end of chamber 66, as can be seen, communicates with the interior of the tank Within which the valve 30 is mounted. To assure an unrestricted flow of fuel from the tank into the valve, chamber 66 is provided with a plurality of circumferentially spaced apart openings 120 in the side wall thereof.
  • the invention proved to be rugged in construction, reliable in operation, and was economically manufactured. It was found that no interruption in fuel tiow occurred when transition of flow from one tank to another took place. r[he tanks emptied one at a time as described hereinabove, substantially all of the fuel being withdrawn from one tank before any was withdrawn from the next succeeding tank.
  • a fuel tank transfer system for an engine compris ⁇ ing in combination a plurality of connected fuel storage tanks, each such storage tank having a fuel port and fuel outlet therein, and each tank including a fioat operated valve, each such float operated valve comprising a first valve seat communicating between the outlet of its tank and the port of its tank, and a movable valve element including a first valve face adapted to cooperate with said first valve seat, a second valve seat communicating between the outlet of said its tank and the interior of said its tank, a movable valve element including a second valve face adapted to cooperate with said second valve seat, iioat means operatively connected to the first said movable valve element to move Isaid first valve face into contact with said first valve seat when said fioat means is urged upwardly by the fuel in said tank and out of contact with said first valve seat when said fioat means is moved downwardly thereby allowing fuel to flow from said port to said outlet when the level in said tank falls below the level of said float means, said oat means operatively connected
  • a fuel tank transfer system for an engine comprising in combination at least first and second fuel storage tanks, each of said tanks having an outlet connection and an inlet connection, a first fuel line connecting the first tank fuel outlet connection to the engine, a pump connected to said first fuel line for moving fuel from said rst tank through said first tank outlet connection and fuel line to the engine, and a second fuel line connecting the second tank outlet connection to the first tank inlet connection, said first and second tanks each including therein a valve housing having first and second inlet open' ings and an outiet opening, a first duct connecting the outlet opening to the tank outlet connection, a second duct connecting the first tank inlet connection to the second inlet opening, the first inlet opening being open to the tank interior, valve means within the valve housing movable between a first position opening the first inlet opening to and closing the second inlet opening to the outlet opening and a second position opening the second inlet opening to and closing the first inlet opening to the loutlet opening, and a float exposed to fuel in the tank and operative
  • each said valve housing is provided with a first annular valve seat between the first inlet opening and the outlet opening and a second annular valve seat between the second inlet opening and the outlet opening, said seats being coaxially aligned, and said valve means in each housing including an elongated valve element extending concentrically through said Seats and having first and second axially spaced valve heads thereon for respective sealing engagement with the first valve seat in said second position and with the second valve seat in said first position.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Ocean & Marine Engineering (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Description

Nov. 24, 1964 G. R. ANDERSON FUEL SUPPLY SYSTEM Filed July 14, 1961 PIE'. 1
N w. s R@ mw 0E 0 T0 f m f V4 an 4 m. .K N M M E a rv I MM2 Y F a a/5B .w 84, 6,2 a, 06 465566 2 MV i l m w 6/ Mtb, Il |168 2 0 M 4 7 0 fe n sa u 7 0 a. n L m 4 88 26 Zd' 6 2 oo E 2 /fffas 4 \\V 1, 2 n
Vl l nav. 9 E- a//Tl v/LI I I 4\ ,k/lo Fyfww M; u 7
United States Patent O 3,158,193 FUEL SUPPLY SYSTEM Glenn R. Anderson, Minneapolis, Minn., assigner to Mc- Culloch Corporation, Scott Division, Minneapolis, Minn., a corporation of Minnesota i Filed July 14, 1961, Ser. No. 124,047 3 Claims. (Cl. 15th-36.3)
This invention relates to fuel supply systems and storage tanks-and more particularly to apparatus enabling fuel to be withdrawn from a plurality of tanks one at a time.
While the invention is suitable for a variety of applications, it is particularly well sui-ted for use in supplying fuel to the motor of a motor boat or the like. Many small boats, such as runab-outs, and the other outboard motor boats do not have enough available space for a single large fuel tank. Thus, for the small boat operator, who cannot employ a single relatively large tank, or the boat operator who must carry gasoline to his boat, it is necessary to keep several small fuel tanks in the boat in order yto run the motor for extended periods of time.
It is, of course, imperative that such tanks be easily carried when filled with fuel. In general, tanks of over yabout six gallons in capacity cannot "be considered portable. When an engine of relatively large horsepower is employed, the -rnotor will often consu-me more than one tank of fuel in a days boating thus requiring the operator to stop, disconnect the fuel rline running from the tank to the motor and transfer the line to a new fuel tank after the fuel in each tank is consumed. This operation is, of course, time consuming and-even more important can be a potential hazard under many boating conditions, for example, in passing a large ship, traveling in heavy currents, or when towing water skiers. Thus, occasionally, when power is most needed, all of the fuel in the tank will be consumed and the motor will stop.
Automatic tank transfer systems have been previously -proposed and have come into relatively common use in aircraft.V However, as far as I am aware, none of such tank transfer systems are satisfactory for the purpose of my invention. Many such systems require pressurization of the fuel tank in order to withdraw fuel therefrom.
In applications such as boating, it is impractical as well as hazardous to pressurize the tanks. Moreover, the tanks must be portable, independently movable, and easily detachable. VThe required valves must be relatively simple in construction and low in cost in order to be of practical value. Moreover, the redirecting or transfer of flow from one tank to the next must be entirely automatic, reliable in operation and must not cause interruption of fuel flow during the transition period. Furthermore, for several reasons it is desirable to empty each of the tanks entirely before -any fuel is Withdrawn from one of the other tanks. First, because evaporation of Volatile fractions from the fuel in a half emptied tank `will cause the remaining fuel to become stale, second, because fire hazards will be reduced and third, because it will then be unnecessary to partially fill all of the tanks each time the boat is used. Thus, according to the present invention, some of the tanks may still be completely full after `an extended run and only the others need be filled.
It is thus an important object of the present invention to provide an improved tank transfer system wherein fuel is stored in a plurality of tanks and withdrawn from such tanks one after -another in succession and wherein each such tank is completely emptied before fuel is withdrawn from one of the other tanks. n
It is another object of this invention to provide an improved fuel transfersys'tem wherein lfuel can be Withdrawn from successive tanks by a single pump connected between the tanks and the engine or 'other device requirngfuelr and wherein no pressurization in the tanks is required to assist in withdrawing fuel from the tanks.
It is another object of this invention to provide an improved fuel and storage transfer system wherein fuel is .withdrawn `from a plurality of fuel storage tanksone at a time and wherein transition of withdrawal from one tank -to one of the other tanks will take place without interrupting the flow ofl fuel.
t is still another object of this invention to provide an improved fuel transfer system employing a plurality of similar portable interchangeable fuel tanks each including a fuel transfer valve therein and wherein said valve is relatively simple in construction and low-in cost.
Briefly stated, the present invention provides a fuel tank transfer system including a plurality of separate independently movable or permanently fixed storage tanks. Each of the tanks has .an open fuel inlet connection and an open fuel outlet connection and each tank includes a float operated valve. This valve is preferably contained within the tank. `Each of the float operated valves includes a second valve seat communicating between the inlet connection and outlet connection of the tank. A movable valve element provided in the valveincludes a second 'valve head adapted to cooperate with the second valve seat. A first valve seat communicates with the outlet connection of the tank and the interior of the tank. A movable valve element including a first valve face is adapted to cooperate with the first valve seat.
For simplicity of construction, it is preferred that a single movable element be used. p
A float is operatively connected to each movable valve lelement to move the second valve face into contact with the second valve seat when the float is urged upwardly by the fuel in said tank and out of contact with the second valve seat when the float is moved downwardly thereby allowing fluid to flow from the tank inlet connection to lthe tank outlet connection when the level in the fuel falls below the level of the float.
A float is operatively connected to the first said movable valve element to move said first valve face onto the said `rst valve seat when the second valve face is out of Contact with the vsaid second valve seatl and away from Vsaid first valve seat when the second valve face is in tanks is adapted to be connected to an engineV or to other device requiring fuel.
` Specifically, each of the tanks includes a valve vcomprising a housing having two inlet openings therein and a single outlet opening. One of these inletopenings communicates with the interior of the tank and the other of y said inlet openings is adapted to be connected to the outlet connection of one of the other of the tanks. .i
v During operation, fuel is selectively withdrawn from each of the tanks in succession. As each tank is emptied, fuel is then withdrawn-from the next adjacent or succeeding tank responsive to thelowering of the float as the last portion of the fuel is drawn from-the tank and without an interruption of the flow of fuel during the time this transition is made. i Y
According to a preferred form of the invention, the valve comprises a housing having an opening or bore therethrough with' first and second spaced .apartr valve seats therein. Each of these Valve seats is provided with a valve port or opening therein. The bore is divided i bore disposed vertically so that one of the end chambers comprises an upper end chamber and other of the end chambers comprises a lower end chamber, the lower end chamber communicating with the interior of the tank and the upper end chamber communicating with the inlet connection of the tank. The outlet connection of the tank communicates with the central chamber.
When a single movable valve element is used, it is preferably slidably mounted within the bore and is provided with a valve head at each end. The valve heads are preferably positioned within said central chamber, in which case, the float can be rigidly connected to the lower end of the movable valve element. If desired, the valve heads can be spaced apart and each positioned in one of the end chambers and in this instance the oat is preferably connected to one end of a lever arm, the other end of which is operatively connected to the lower end of the movable valve element.
The inventionwill be best understood by reference to the specification which sets forth a preferred form of the invention and to the drawings wherein- FIG. 1 is a vertical longitudinal sectional view of a boat and motor utilizing the present invention. ,p
FIG. 2 is a semi-diagrammatic vertical sectional view of the fuel transfer system according to the present invention.
FIG. 3 is a vertical sectional view of a fuel iiow transfer valve of the present invention.
FIG. 4 is a vertical sectional view of another form of iiow transfer valve of the present invention.
Referring now to the drawings, there is shown in FIG. 1 a boat 10 and motor 12 secured to the transom 14 of the boat 10. Means for transferring or pumping fuel comprises a fuel pump 16 secured to the motor 12. A pump outlet duct 18 is connected between the outlet of pump 16 and the carburetor (not shown) of the motor 12. The inlet of the pump 16 is provided with a quick disconnect coupling 20 of known construction.
A yplurality of similar interchangeable portable fuel tanks 22 provide fuel for the engine 12. While any number of such tanks can be used, three such tanks are shown by way of example. Each of the tanks 22 is provided with an open inlet connection 24 and an open outlet connection 26, a removable lill cover 28, a fuel transfer valve 30 within the tank and carrying handle 32 connected to the upper surface of the tank.
The inlet connection 24 and outlet connection 26 of each of tanks 22 are preferably provided with quick disconnect couplings 34. A duct or line 36 is secured between the inlet connection 26 of the tank 22 at the left in FIGS. l and 2, and the pump 16. Another fuel duct or line 37 is secured between the inlet connection of the same tank and the outlet connection 26 of the center tank of FIGS. l and 2. A similar fuel line or duct 38 is connected between the inlet connection of the latter tank and the outlet connect-ion of the tank 22 at the right of FIGS. l and 2. The lines 36, 37 and 38 may be easily and quickly disconnected at either end thereof when it is desired to fill the tanks or remove them from the boat. The tanks, of course, are lilled through the opening cover by the ll cap 2S.
Connected between the inlet connection 24 and the valve 30 of each tank 22 is an inlet duct 42 and connected between the outlet connection 26 and each of valves 30 is an outlet duct 44.
The tanks are thus connected together in series, the outlet of one tank, being connected to the inlet of the next adjacent tank and as many tanks as required can be thus connected together in series.f It is understood, however, that the inletv connection of the trank at the end of sucha series of tanks will have no fuel line connected thereto and also. the tank at the opposite end of such a vseries of tanks-will have its outlet connection connected to the inlet. of the enginel 12.
Ducts 42 and 44 are preferably metal conduits which in addition to serving as fuel lines are used to position the valve 30 securely within the tank. As shown in FIG. 2, the valve 30 is positioned at the bottom of the tank 22 with the lower end thereof against the lower surface of tank 22.
Reference is now made to FIGS. 3 and 4 which show two valves 30 according to the present invention. These valves'are similar in construction except as described hereinbelow; The valves 30 include a housing 48 which is cylindrical in crosslsection and of somewhat greater height than width. The housing 48 is provided with a vertically extending opening or bore S0 therein which extends from one end to the other. The bore 50 is provided with a reduced diameter to form a irst valve seat 52 and a first valve port 54. The bore 50 is screw threaded at 56 to receive a removable valve seat member 58. Valve seat member 58 includes a second valve port 6G and second valve seat 62.
The first and second valve seats 52 and 62 respectively divide the bore 50 into a pair of end chambers 64 and 66 and a central chamber 68 between the valve seats 52 and 62. The valve chamber 64 comprises an upper valve chamber and the valve chamber 66 comprises a lower valve chamber. The upper end of the bore 50 is screw threaded at 70 to receive an adapter '72 to which the inlet duct 42 is secured. The adapter 72 is provided with an opening 74 therein to allow communication between the duct 42 and the upper chamber 64.
The housing 48 is bored and threaded at 76 to receive an adapter 78 to which the outlet duct 44 `is secured.
The adapter 78 is provided with an opening 80 to allow communication between the outlet duct 44 and the central chamber 68.
Referring now particularly to FIG. 3, -it will be seen that the valve Sil is provided with a movable valve element 82. While the movable valve element may be conystructed in various ways, according to one form of the invention, it comprises a shaft 84 concentrically and slidably mounted within the bore 50 and extending through the ports 60 and 54. Shaft 84 is of a sufliciently y small diameter so that it will not obstruct the flow of fuel through the ports '54. and 60. Secured rigidly to shaft 84 and positioned within the central chamber 68 is a valve sealing element 86 preferably formed from resilient material such as rubber. The valve sealing element 86 includes a first valve head 88 at .the lower end thereof and a second valve head 90 at the upper end thereof. Each valve head includes a frustoconical valve face and the valve face of the lower valve head 88 is adapted to cooperate with and seal the first valve seat 52 while the upper valve head 90, and its valve face, are
adapted to cooperate with and seal the second valve seat 62.
Operatively connected to the movable valve element 82 isa iloat 92.. According to the form of the invention shown vin FIG. 3, the oat 92 is rigidly secured to the lower end of the shaft 84 and is 4entirely contained within the chamber 66. Thus, as can be lseen in the figures, when the level of the fuel within the tank 22 is above the float 92, the float 92 will rise causing the upper valve head 90 and its valve face to seal the valve seat 62 andthus close the port 6B. When the level of fuel falls below the tioat V92, the oat will lower causing the rnovable'valve.v element 82 to lower and thereby causing the lower head Acentrically within the bore 50 and movable longitudinally of the bore. Shaft' 192 has mounted concentrically thereon at the upper and lower ends thereof a pair of spaced apart valve heads 104 and 166. The valve heads 104 and 105 are secured to the shaft 102 rigidly by any suitable means such as adhesive and they are preferably formed from a resilient material, such as rubber. Each of the valve heads 104 and 1% is spaced outwardly of the valve ports 54 and 6i?, the lower valve head 104i being adapted to cooperates with an seal the valve seat 52 of port 54 and the upper valve 106 1oeing adapted to cooperate with and seal the port e0 of valve seat 52. Each of the valve heads 104 and 106 are provided with tapered or frustoconical valve faces adapted to seat against the respective valve seats.
Pivotally connected to the lower end of the housing 4S by means of a horizontal pivot pin 108 is a lever arm 110. Connected to the outward end of lever arm 110 is a iioat 112. The opposite end of lever arm 110 is operatively connected by any suitable means to the lower end of the movable valve element 100. For purposes of example, this connection is shown as a il-shaped fork 113 including a pair of prongs which extend on either side of the shaft 102. A pair of spaced apart stops 116 and 11S are provided on shaft 102 to limit the upward and downward movement of the fork 113 thereon. Thus, when the iioat 112 moves downwardly, the movable valve element 1d@ will move upwardly thereby causing the lower valve head 104 to seat against the lower valve seat 52 thereby closing port 54. When the float 112 moves upwardly, movable valve element 100 will move downwardly causing the valve head 111% to seal port of?.
In the valves of both FTGS. 3 and 4, the lower end of chamber 66, as can be seen, communicates with the interior of the tank Within which the valve 30 is mounted. To assure an unrestricted flow of fuel from the tank into the valve, chamber 66 is provided with a plurality of circumferentially spaced apart openings 120 in the side wall thereof.
For purposes of describing the operation of the invention, it will be assumed that all of the tanks arelled with fuel. With all of the tank filled, the float of each valve will be raised causing the upper valve face to seal the port 60 of each of the valves. The fuel will be drawn through line 36 from line 44 and from the chamber 66 of the valve 30 of the tank, at the left of FIGS. 1 and 2. Thus, tank 22 at the left in the figures, will be emptied first. When the float of the valve 30 in this tank is lowered, fuel will then be withdrawn from the next succeeding tank viz. the center tank of FIGS. 1 and 2. This o eration is repeated until all of the tanks are emptied.
Under conditions of actual use, the invention proved to be rugged in construction, reliable in operation, and was economically manufactured. It was found that no interruption in fuel tiow occurred when transition of flow from one tank to another took place. r[he tanks emptied one at a time as described hereinabove, substantially all of the fuel being withdrawn from one tank before any was withdrawn from the next succeeding tank.
It is understood that suitable modifications may be made inthe structure as disclosed, provided such modifications come within the spirit and scope of the appended claims. Having now therefore fully illustrated and described rny invention, what 1 claim to be new and desire to protect by Letters Patent is:
1. A fuel tank transfer system for an engine compris` ing in combination a plurality of connected fuel storage tanks, each such storage tank having a fuel port and fuel outlet therein, and each tank including a fioat operated valve, each such float operated valve comprising a first valve seat communicating between the outlet of its tank and the port of its tank, and a movable valve element including a first valve face adapted to cooperate with said first valve seat, a second valve seat communicating between the outlet of said its tank and the interior of said its tank, a movable valve element including a second valve face adapted to cooperate with said second valve seat, iioat means operatively connected to the first said movable valve element to move Isaid first valve face into contact with said first valve seat when said fioat means is urged upwardly by the fuel in said tank and out of contact with said first valve seat when said fioat means is moved downwardly thereby allowing fuel to flow from said port to said outlet when the level in said tank falls below the level of said float means, said oat means operatively connected to the second said movable valve element adapted to move said second valve face onto said second valve seat when said first valve face is out of contact with said first Valve seat and out of contact with said second valve seat when said first valve face is in contact with said first valve seat and duct means connecting the outlet of one of said tanks to said engine and the port thereof to the outlet of another of said tanks.
2. A fuel tank transfer system for an engine comprising in combination at least first and second fuel storage tanks, each of said tanks having an outlet connection and an inlet connection, a first fuel line connecting the first tank fuel outlet connection to the engine, a pump connected to said first fuel line for moving fuel from said rst tank through said first tank outlet connection and fuel line to the engine, and a second fuel line connecting the second tank outlet connection to the first tank inlet connection, said first and second tanks each including therein a valve housing having first and second inlet open' ings and an outiet opening, a first duct connecting the outlet opening to the tank outlet connection, a second duct connecting the first tank inlet connection to the second inlet opening, the first inlet opening being open to the tank interior, valve means within the valve housing movable between a first position opening the first inlet opening to and closing the second inlet opening to the outlet opening and a second position opening the second inlet opening to and closing the first inlet opening to the loutlet opening, and a float exposed to fuel in the tank and operatively connected to the valve means therewith to -hold the valve means in the first position while fuel remains in the tank but to move the valve means to the second position when fuel has been substantially drained from the tank.-
3. The subject matter of claim 2 wherein each said valve housing is provided with a first annular valve seat between the first inlet opening and the outlet opening and a second annular valve seat between the second inlet opening and the outlet opening, said seats being coaxially aligned, and said valve means in each housing including an elongated valve element extending concentrically through said Seats and having first and second axially spaced valve heads thereon for respective sealing engagement with the first valve seat in said second position and with the second valve seat in said first position.
References Cited in the file of this patent UNITED STATES PATENTS 849,048 Cable Apr. 2, 1907 1,909,390 Ballet al May 16, 1933 2,024,548 Struve Dec. 17, 1935 2,146,729 Gavin Feb. 14, 1939 2,660,188 McCartney Nov. 24, i953 3,020,030 Capehart Feb. 6, 1962

Claims (1)

1. A FUEL TANK TRANSFER SYSTEM FOR AN ENGINE COMPRISING IN COMBINATION A PLURALITY OF CONNECTED FUEL STORAGE TANKS, EACH SUCH STORAGE TANK HAVING A FUEL PORT AND FUEL OUTLET THEREIN, AND EACH TANK INCLUDING A FLOAT OPERATED VALVE, EACH SUCH FLOAT OPERATED VALVE COMPRISING A FIRST VALVE SEAT COMMUNICATING BETWEEN THE OUTLET OF ITS TANK AND THE PORT OF ITS TANK, AND A MOVABLE VALVE ELEMENT INCLUDING A FIRST VALVE FACE ADAPTED TO COOPERATE WITH SAID FIRST VALVE SEAT, A SECOND VALVE SEAT COMMUNICATING BETWEEN THE OUTLET OF SAID ITS TANK AND THE INTERIOR OF SAID ITS TANK, A MOVABLE VALVE ELEMENT INCLUDING A SECOND VALVE FACE ADAPTED TO COOPERATE WITH SAID SECOND VALVE SEAT, FLOAT MEANS OPERATIVELY CONNECTED TO THE FIRST SAID MOVABLE VALVE ELEMENT TO MOVE SAID FIRST VALVE FACE INTO CONTACT WITH SAID FIRST VALVE SEAT WHEN SAID FLOAT MEANS IS URGED UPWARDLY BY THE FUEL IN SAID TANK AND OUT OF CONTACT WITH SAID FIRST VALVE SEAT WHEN SAID FLOAT MEANS IS MOVED DOWNWARDLY THEREBY ALLOWING FUEL TO FLOW FROM SAID PORT TO SAID OUTLET WHEN THE LEVEL IN SAID TANK FALLS BELOW THE LEVEL OF SAID FLOAT MEANS, SAID FLOAT MEANS OPERATIVELY CONNECTED TO THE SECOND SAID MOVABLE VALVE ELEMENT ADAPTED TO MOVE SAID SECOND VALVE FACE ONTO SAID SECOND VALVE SEAT WHEN SAID FIRST VALVE FACE IS OUT OF CONTACT WITH SAID FIRST VALVE SEAT AND OUT OF CONTACT WITH SAID SECOND VALVE SEAT WHEN SAID FIRST VALVE FACE IS IN CONTACT WITH SAID FIRST VALVE SEAT AND DUCT MEANS CONNECTING THE OUTLET OF ONE OF SAID TANKS TO SAID ENGINE AND THE PORT THEREOF TO THE OUTLET OF ANOTHER OF SAID TANKS.
US12404761 1961-07-14 1961-07-14 Fuel supply system Expired - Lifetime US3158193A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US12404761 US3158193A (en) 1961-07-14 1961-07-14 Fuel supply system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12404761 US3158193A (en) 1961-07-14 1961-07-14 Fuel supply system

Publications (1)

Publication Number Publication Date
US3158193A true US3158193A (en) 1964-11-24

Family

ID=22412441

Family Applications (1)

Application Number Title Priority Date Filing Date
US12404761 Expired - Lifetime US3158193A (en) 1961-07-14 1961-07-14 Fuel supply system

Country Status (1)

Country Link
US (1) US3158193A (en)

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3331392A (en) * 1964-10-15 1967-07-18 Andrew D Davidson Clear plastic fuel manifold
US3409040A (en) * 1965-06-02 1968-11-05 Robert L Weston Fuel supply system for internal combustion engine
US3739803A (en) * 1971-06-11 1973-06-19 Pirelli Oil compensation system for electric power cables impregnated with insulating oil
US3896972A (en) * 1973-07-09 1975-07-29 Samuel W Neidore Remote liquid distribution system
US4602599A (en) * 1984-07-09 1986-07-29 Glagola Mark E Emergency fuel priming and supply system for engines
US4653552A (en) * 1985-09-25 1987-03-31 Outboard Marine Corporation Fuel tank cap
US4807582A (en) * 1986-11-07 1989-02-28 Walbro Corporation Reserve fuel shut-off valve
US5035346A (en) * 1988-03-10 1991-07-30 Vegyimuveket Epito Es Szerelo Vallalat United liquid-level and pressure regulator for separators
US5303728A (en) * 1992-08-10 1994-04-19 Donald Senatore Water conservation system
US6318644B1 (en) 1997-05-15 2001-11-20 Ronnie Joe Weiand Fluid transfer pump wash-out apparatus and method
US20050166967A1 (en) * 2004-01-29 2005-08-04 Howe Mark E. Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20060086387A1 (en) * 2004-10-21 2006-04-27 Amit Gupta Continuous chemical feeder and method of use thereof
US20060214061A1 (en) * 2004-01-29 2006-09-28 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20060214060A1 (en) * 2004-01-29 2006-09-28 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20070096452A1 (en) * 2005-10-24 2007-05-03 Yamaha Hatsudoki Kabushiki Kaisha Fuel Tank Assembly and Straddle-Type Vehicle Having the Same
US20080035216A1 (en) * 2006-08-14 2008-02-14 Graeve Theodore H Water supply system
US8356618B1 (en) * 2009-04-21 2013-01-22 Werner Todd C Water separator for small boat fuel systems
FR2978119A1 (en) * 2011-07-22 2013-01-25 Stx France Sa SHIP EQUIPPED WITH FUEL STORAGE SYSTEM AND CORRESPONDING METHOD
US20150122939A1 (en) * 2013-11-05 2015-05-07 Airbus Helicopters Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle floor of the fuselage of the rotorcraft
EP2157014A4 (en) * 2007-05-18 2015-08-19 Ihi Corp Fuel supply method and device for internal combustion marine engine
EP3130540A1 (en) * 2015-08-12 2017-02-15 The Boeing Company Tanker aircraft capacity extension system and method
US10040345B2 (en) 2013-10-16 2018-08-07 Kenneth S. Anderson Spare tire fuel tank
US11427076B1 (en) * 2018-08-10 2022-08-30 Matt Rocco Portable fuel tank configured to be releasably secured
US20230020034A1 (en) * 2021-07-16 2023-01-19 Yamaha Hatsudoki Kabushiki Kaisha Fuel management system capable of freely performing transfer of fuel among a plurality of fuel tanks

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US849048A (en) * 1906-10-08 1907-04-02 Electric Boat Co Fuel-feed for hydrocarbon-engines.
US1909390A (en) * 1930-09-10 1933-05-16 Chrysler Corp Antipercolating device
US2024548A (en) * 1935-12-17 Oil feeding and control tank for
US2146729A (en) * 1938-04-11 1939-02-14 Edward M Gavin Automatic fuel control system for vehicles
US2660188A (en) * 1952-05-12 1953-11-24 Mccartney Engineering & Res Co Automatic tank valve for flow lines
US3020030A (en) * 1959-12-09 1962-02-06 Capehart Zbitnoff Corp Carburetor device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2024548A (en) * 1935-12-17 Oil feeding and control tank for
US849048A (en) * 1906-10-08 1907-04-02 Electric Boat Co Fuel-feed for hydrocarbon-engines.
US1909390A (en) * 1930-09-10 1933-05-16 Chrysler Corp Antipercolating device
US2146729A (en) * 1938-04-11 1939-02-14 Edward M Gavin Automatic fuel control system for vehicles
US2660188A (en) * 1952-05-12 1953-11-24 Mccartney Engineering & Res Co Automatic tank valve for flow lines
US3020030A (en) * 1959-12-09 1962-02-06 Capehart Zbitnoff Corp Carburetor device

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3331392A (en) * 1964-10-15 1967-07-18 Andrew D Davidson Clear plastic fuel manifold
US3409040A (en) * 1965-06-02 1968-11-05 Robert L Weston Fuel supply system for internal combustion engine
US3739803A (en) * 1971-06-11 1973-06-19 Pirelli Oil compensation system for electric power cables impregnated with insulating oil
US3896972A (en) * 1973-07-09 1975-07-29 Samuel W Neidore Remote liquid distribution system
US4602599A (en) * 1984-07-09 1986-07-29 Glagola Mark E Emergency fuel priming and supply system for engines
US4653552A (en) * 1985-09-25 1987-03-31 Outboard Marine Corporation Fuel tank cap
US4807582A (en) * 1986-11-07 1989-02-28 Walbro Corporation Reserve fuel shut-off valve
US5035346A (en) * 1988-03-10 1991-07-30 Vegyimuveket Epito Es Szerelo Vallalat United liquid-level and pressure regulator for separators
US5303728A (en) * 1992-08-10 1994-04-19 Donald Senatore Water conservation system
US6318644B1 (en) 1997-05-15 2001-11-20 Ronnie Joe Weiand Fluid transfer pump wash-out apparatus and method
US20050166967A1 (en) * 2004-01-29 2005-08-04 Howe Mark E. Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20060214061A1 (en) * 2004-01-29 2006-09-28 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20060214060A1 (en) * 2004-01-29 2006-09-28 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US7357355B2 (en) 2004-01-29 2008-04-15 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US7568660B2 (en) 2004-01-29 2009-08-04 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US7357149B2 (en) * 2004-01-29 2008-04-15 The Boeing Company Auxiliary fuel tank systems for aircraft and methods for their manufacture and use
US20060086387A1 (en) * 2004-10-21 2006-04-27 Amit Gupta Continuous chemical feeder and method of use thereof
WO2006047224A3 (en) * 2004-10-21 2006-12-21 Nalco Co Continuous chemical feeder and method of use thereof
US7201178B2 (en) * 2004-10-21 2007-04-10 Nalco Company Continuous chemical feeder and method of use thereof
US20070096452A1 (en) * 2005-10-24 2007-05-03 Yamaha Hatsudoki Kabushiki Kaisha Fuel Tank Assembly and Straddle-Type Vehicle Having the Same
US7484766B2 (en) * 2005-10-24 2009-02-03 Yamaha Hatsudoki Kabushiki Kaisha Fuel tank assembly and straddle-type vehicle having the same
US20080035216A1 (en) * 2006-08-14 2008-02-14 Graeve Theodore H Water supply system
US7631658B2 (en) 2006-08-14 2009-12-15 Graeve Jr Theodore H Water supply system
EP2157014A4 (en) * 2007-05-18 2015-08-19 Ihi Corp Fuel supply method and device for internal combustion marine engine
US8356618B1 (en) * 2009-04-21 2013-01-22 Werner Todd C Water separator for small boat fuel systems
FR2978119A1 (en) * 2011-07-22 2013-01-25 Stx France Sa SHIP EQUIPPED WITH FUEL STORAGE SYSTEM AND CORRESPONDING METHOD
WO2013014020A1 (en) * 2011-07-22 2013-01-31 Stx France S.A. Ship provided with a fuel storage system, and corresponding method
US10040345B2 (en) 2013-10-16 2018-08-07 Kenneth S. Anderson Spare tire fuel tank
US20150122939A1 (en) * 2013-11-05 2015-05-07 Airbus Helicopters Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle floor of the fuselage of the rotorcraft
US9868544B2 (en) * 2013-11-05 2018-01-16 Airbus Helicopters Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle floor of the fuselage of the rotorcraft
US9873519B2 (en) 2015-08-12 2018-01-23 The Boeing Company Tanker aircraft capacity extension system and method
EP3130540A1 (en) * 2015-08-12 2017-02-15 The Boeing Company Tanker aircraft capacity extension system and method
US11427076B1 (en) * 2018-08-10 2022-08-30 Matt Rocco Portable fuel tank configured to be releasably secured
US20230020034A1 (en) * 2021-07-16 2023-01-19 Yamaha Hatsudoki Kabushiki Kaisha Fuel management system capable of freely performing transfer of fuel among a plurality of fuel tanks
US11939033B2 (en) * 2021-07-16 2024-03-26 Yamaha Hatsudoki Kabushiki Kaisha Fuel management system capable of freely performing transfer of fuel among a plurality of fuel tanks

Similar Documents

Publication Publication Date Title
US3158193A (en) Fuel supply system
US2594105A (en) System for gathering and loading oil from underwater oil wells
US4300489A (en) Pipe closing device
US4037992A (en) Slurry continuous pressure-feeding apparatus
GB1275987A (en) Improvements in or relating to floating columns for oil drilling installations
US3109294A (en) Storage tank and liquid flow control means
US4715309A (en) Device for the handling of liquids
US2320913A (en) Liquid fuel or lubricant supply tank
WO2019000798A1 (en) Topside ballast tank ballast water bleed-off system
US1831318A (en) Float operated valve
US3957009A (en) Ship ballast, oil and water separation system
DE1956472U (en) SUPPORTING BASE FOR COMBUSTION MACHINES, IN PARTICULAR FOR ROTARY LISTON MACHINES.
GB1038507A (en) Float valve
US3379404A (en) Control system
EP0130066A2 (en) Method and system for producing natural gas from offshore wells
US4223622A (en) Tanker desludging system
US1342874A (en) Float-valve mechanism
US1865387A (en) Automatic shut-off for tanks
US1602279A (en) Line valve
US2259633A (en) Fuel separator
US2712795A (en) Pneumatic-hydraulic pressure device
US1380575A (en) Means for automatically registering a ship's draft
US3134388A (en) Marine engine flushing
US3905724A (en) Pneumatic pump
CN2145894Y (en) Oil-water separating valve