US2320913A - Liquid fuel or lubricant supply tank - Google Patents

Liquid fuel or lubricant supply tank Download PDF

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Publication number
US2320913A
US2320913A US395657A US39565741A US2320913A US 2320913 A US2320913 A US 2320913A US 395657 A US395657 A US 395657A US 39565741 A US39565741 A US 39565741A US 2320913 A US2320913 A US 2320913A
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Prior art keywords
tank
liquid
pipe
stand
compartments
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Expired - Lifetime
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US395657A
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Thomas W Crowell
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B27/00Arrangement of ship-based loading or unloading equipment for cargo or passengers
    • B63B27/24Arrangement of ship-based loading or unloading equipment for cargo or passengers of pipe-lines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K15/077Fuel tanks with means modifying or controlling distribution or motion of fuel, e.g. to prevent noise, surge, splash or fuel starvation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/14Filling or emptying
    • B64D37/20Emptying systems
    • 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
    • Y10T137/4841With cross connecting passage
    • 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
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7837Direct response valves [i.e., check valve type]
    • Y10T137/7904Reciprocating valves
    • Y10T137/7908Weight biased
    • Y10T137/7909Valve body is the weight
    • Y10T137/7913Guided head

Definitions

  • This invention relates to a liquid fuel or lubricant supply tank for engines, and is especially adapted for use on any kind of land, water or air vehicle, and has for the primary object the provision of a -device of this character which,
  • Figure l is a side elevation partly in section illustrating a liquid storage tank constructed in accordance with my invention.
  • Figure 2 is a sectional view taken on the line '1?2 of Figure l.
  • Figure 3 is a fragmentary vertical sectional view illustrating one of the check valves.
  • Figure 4 is a plan View illustrating the movable element of the check valve.
  • the numeral 5 indicates a liquid tank constructed of any material suitable for the purpose and of any selected size.
  • the tank 5 includes vertical walls 6, a top wall 'I, and a bottom wall 8. Said walls may be of integral construction or secured together in any well known manner so as to render the tank leak-proof.
  • partitions 9 and I0 Arranged within the tank are transverse and longitudinally extending partitions 9 and I0 dividing said tank into a plurality of liquid compartments II.
  • the partitions may be joined onto the walls of the tank in any well known manner so that said compartments will each be leak-proof and noncommunicative except at their upper ends in close proximity to the top wall I of the tank.
  • the partitions 9 and IG are ported, as shown at I2, so that in filling the tank from a common fill spout I 3 the overflow from one compartment to another may be accomplished for the purpose of filling each compartment to a selected level.
  • the location of the ll spout I3 may be varied to suit diil'erent requirements or application of the tank to different devices.
  • a closure cap Ill is provided for the fill spout.
  • the tank 5 is provided with a stand-pipe I5 arranged interiorh7 thereof or exteriorly if desired.
  • the stand-pipe I5 is shown in the drawing as being arranged within one of the compartments and terminates at its upper end adjacent the top wall 'I of the tank.
  • the stand-pipe adjacent its lower end is shouldered, as shown at I6, to rest upon the bottom Wall 8 of the tank while the lower screw threaded end I'I thereof extends through an opening provided in the bottom wall 8 and has threaded thereon a packing nut I8 to engage with the bottom wall and cooperate with the shoulder I6 in providing a leak-proof connection bet-Ween the stand-pipe and the tank.
  • the lower screw threaded end I'I of the standpipe which is arranged exteriorly of the tank has a liquid line or pipe I9 connected thereto for the purpose of conveying the liquid of the tank to an engine.
  • a plurality of branch pipes 2U are connected with the stand-pipe I5 a limited distance above the bottom wall 8 of the tank and extends into the various compartments terminating in downwardly directed ends 2I to which are connected check valves 22 that will permit liquid from the compartments to flow to the stand-pipe but which will prevent the liquid from re-entering the compartments from the stand-pipe.
  • Check valves 22 of a conventional construction are arranged in the branch pipes 20, so that should any one of said branch pipes be broken at the line of drainage to any one of the compartments, the flow of liquid from the stand-pipe and any of the undamaged compartments will be prevented from wasting from the damaged compartment and the damaged portion of the branch pipe.
  • Each check valve 22 consists of a substantially cup-shaped housing 23 having a reduced screw threaded end 24 for connection with a branch pipe.
  • the other end of the cup-shaped housing is internally screw threaded to receive a ported plug 25, acting as a seat for a check valve element 26 in the form of a disc having its periphery provided with a series of notches 21.
  • the cup-shaped housing 23 is provided with an internal shoulder 28 acting to limit the distance in which the valve element 26 may move oi its seat and when disengaged from said seat liquid may ow into the housing 23 by passing through the various notches 2l and the ported plug 25.
  • a gauge rod 29 may extend through the top Wall 'l of the tank and enter the upper portion of the stand-pipe and is equipped with a oat 3l) adapted to move the gauge rod 29 in accordance with the level of the liquid within the tank and consequently permit a person to readily determine the approximate amount of liquid in said tank.
  • the stand-pipe I5 When the stand-pipe I5 is located exteriorly of the tank it is secured thereto in any well known manner and the various branch pipes 22 connected thereto and leading to the various compartments may enter certain walls of the tank.
  • the tank may be constructed of any material suitable for the purpose and its design or shape may be varied to facilitate its installation, as for instance, the tank may be of such a shape that it may be installed in a wing of an aeroplane or some other type of ying machine.
  • a tank In a liquid supply for engines, a tank, a plurality of connected partitions dividing the tank into a plurality of compartments and each partition having an opening connecting said compartments with each other adjacent an upper wall of the tank, a stand pipe located in one of the compartments and including means for connecting thereof to an engine and extending through the bottom wall of the tank, branch pipes connected with the stand pipe adjacent the lower end thereof and each having a free end portion curved to extend downwardly and terminating within a compartment at a selected dista-nce above the bottom wall of the tank, a cup-shaped depending housing secured on each of said ends of the branch pipes and having an internal shoulder and a screw threaded lower end, a ported plug threaded in each of the housings and spaced in close relation to the bottom wall of the tank, and a notched disc-like valve element operating in each of said housings between the shoulder and the plug to provide a check valve to permit flow of liquid from the compartment to the stand pipe and preventing reverse flow of liquid from the stand-pipe to said compartment and

Description

June 1, 1943. T. w. CROWELL LIQUID FUEL OR LUBRICANT SUPPLY'TANK Filed May 28, 1941 @Halma/13S Patented June 1, 1943 UNITED STATES PATENT OFFICE LIQUlD FUEL R LUBRICANT SUPPLY TANK Thomas W. Crowell, Matthews, N. C. Application May 28, 1941, Serial No. 395,657
1 Claim.
This invention relates to a liquid fuel or lubricant supply tank for engines, and is especially adapted for use on any kind of land, water or air vehicle, and has for the primary object the provision of a -device of this character which,
will provide a maximum amount of storage space for the liquid therein without having its overall size increased over the size of conventional storage tanks employed for the same purpose and will prevent total loss of the liquid should the tank leak from any cause, such as being damaged frorn a collision, vibration or penetration by a bullet or the like, consequently leaving sufiicient fluid therein for the maintenance of operation of the engine until such time that the device employing the engine may be brought to a selected designation.
With these and other objects in view as will become more apparent as the description proceeds, the invention consists in certain novel features of construction, combination and arrangement of parts as will be hereinafter more fully described and claimed.
For a complete understanding of my invention, reference is to be had to the following description and accompanying drawing, in which Figure l is a side elevation partly in section illustrating a liquid storage tank constructed in accordance with my invention.
Figure 2 is a sectional view taken on the line '1?2 of Figure l.
Figure 3 is a fragmentary vertical sectional view illustrating one of the check valves.
Figure 4 is a plan View illustrating the movable element of the check valve.
Referring in detail to the drawing, the numeral 5 indicates a liquid tank constructed of any material suitable for the purpose and of any selected size. The tank 5 includes vertical walls 6, a top wall 'I, and a bottom wall 8. Said walls may be of integral construction or secured together in any well known manner so as to render the tank leak-proof.
Arranged within the tank are transverse and longitudinally extending partitions 9 and I0 dividing said tank into a plurality of liquid compartments II. The partitions may be joined onto the walls of the tank in any well known manner so that said compartments will each be leak-proof and noncommunicative except at their upper ends in close proximity to the top wall I of the tank. The partitions 9 and IG are ported, as shown at I2, so that in filling the tank from a common fill spout I 3 the overflow from one compartment to another may be accomplished for the purpose of filling each compartment to a selected level. The location of the ll spout I3 may be varied to suit diil'erent requirements or application of the tank to different devices.
A closure cap Ill is provided for the fill spout.
The tank 5 is provided with a stand-pipe I5 arranged interiorh7 thereof or exteriorly if desired. However, the stand-pipe I5 is shown in the drawing as being arranged within one of the compartments and terminates at its upper end adjacent the top wall 'I of the tank. The stand-pipe adjacent its lower end is shouldered, as shown at I6, to rest upon the bottom Wall 8 of the tank while the lower screw threaded end I'I thereof extends through an opening provided in the bottom wall 8 and has threaded thereon a packing nut I8 to engage with the bottom wall and cooperate with the shoulder I6 in providing a leak-proof connection bet-Ween the stand-pipe and the tank.
The lower screw threaded end I'I of the standpipe which is arranged exteriorly of the tank has a liquid line or pipe I9 connected thereto for the purpose of conveying the liquid of the tank to an engine.
A plurality of branch pipes 2U are connected with the stand-pipe I5 a limited distance above the bottom wall 8 of the tank and extends into the various compartments terminating in downwardly directed ends 2I to which are connected check valves 22 that will permit liquid from the compartments to flow to the stand-pipe but which will prevent the liquid from re-entering the compartments from the stand-pipe.
Check valves 22 of a conventional construction are arranged in the branch pipes 20, so that should any one of said branch pipes be broken at the line of drainage to any one of the compartments, the flow of liquid from the stand-pipe and any of the undamaged compartments will be prevented from wasting from the damaged compartment and the damaged portion of the branch pipe.
This arrangement of check valves will prevent liquid from flowing from one compartment to another by way of the different branch pipes and the stand-pipe, but as stated, the liquid of any compartment may readily flow to the standpipe for passage therefrom to the engine.
Each check valve 22 consists of a substantially cup-shaped housing 23 having a reduced screw threaded end 24 for connection with a branch pipe. The other end of the cup-shaped housing is internally screw threaded to receive a ported plug 25, acting as a seat for a check valve element 26 in the form of a disc having its periphery provided with a series of notches 21. Further, the cup-shaped housing 23 is provided with an internal shoulder 28 acting to limit the distance in which the valve element 26 may move oi its seat and when disengaged from said seat liquid may ow into the housing 23 by passing through the various notches 2l and the ported plug 25.
A gauge rod 29 may extend through the top Wall 'l of the tank and enter the upper portion of the stand-pipe and is equipped with a oat 3l) adapted to move the gauge rod 29 in accordance with the level of the liquid within the tank and consequently permit a person to readily determine the approximate amount of liquid in said tank.
When the stand-pipe I5 is located exteriorly of the tank it is secured thereto in any well known manner and the various branch pipes 22 connected thereto and leading to the various compartments may enter certain walls of the tank.
Thus it will be seen from the foregoing description taken in connection with the drawing, that a very eiicient supply tank has been provided that may be easily installed in any type of vehicle for the purpose of supplying the engine thereof either with liquid fuel or lubricant. Furthermore it will be seen that should the tank at any given point be damaged as to cause leakage only the compartment where the damage occurs will lose its contents, consequently leaving the liquid within the other compartments undisturbed and useable by the engine.
As before statedy the tank may be constructed of any material suitable for the purpose and its design or shape may be varied to facilitate its installation, as for instance, the tank may be of such a shape that it may be installed in a wing of an aeroplane or some other type of ying machine.
While I have shown and described the preferred embodiment of my invention, it Will be understood that minor changes in construction, combination and arrangement of parts may be made without departing from` the spirit and scope of the invention as claimed.
Having thus described the invention, what I claim as new is:
In a liquid supply for engines, a tank, a plurality of connected partitions dividing the tank into a plurality of compartments and each partition having an opening connecting said compartments with each other adjacent an upper wall of the tank, a stand pipe located in one of the compartments and including means for connecting thereof to an engine and extending through the bottom wall of the tank, branch pipes connected with the stand pipe adjacent the lower end thereof and each having a free end portion curved to extend downwardly and terminating within a compartment at a selected dista-nce above the bottom wall of the tank, a cup-shaped depending housing secured on each of said ends of the branch pipes and having an internal shoulder and a screw threaded lower end, a ported plug threaded in each of the housings and spaced in close relation to the bottom wall of the tank, and a notched disc-like valve element operating in each of said housings between the shoulder and the plug to provide a check valve to permit flow of liquid from the compartment to the stand pipe and preventing reverse flow of liquid from the stand-pipe to said compartment and from one compartment to another.
THOMAS VJ. CROSVELL.
US395657A 1941-05-28 1941-05-28 Liquid fuel or lubricant supply tank Expired - Lifetime US2320913A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2616294A (en) * 1948-12-02 1952-11-04 Claude A Pickens Filtering liquid level gauge
DE937991C (en) * 1953-06-06 1956-01-19 Daimler Benz Ag Fuel tank
US2955787A (en) * 1956-12-27 1960-10-11 Lockheed Aircraft Corp Auxiliary fuel tank
US3001376A (en) * 1957-11-26 1961-09-26 British Oxygen Co Ltd Storage tanks for liquid oxygen and the like in rockets
US3396744A (en) * 1962-12-06 1968-08-13 Leo L. Schwarz System for elimination of condensation in fuel storage tanks
FR2398256A1 (en) * 1977-07-19 1979-02-16 Bayerische Motoren Werke Ag SUCTION STRAINER FOR THE SUCTION TUBING OF A LUBRICANT PUMP
US4655248A (en) * 1985-12-16 1987-04-07 United Technologies Corporation Check valve
US5020566A (en) * 1990-08-13 1991-06-04 Sullair Corporation Fuel supply system for portable engine driven equipment
US5328094A (en) * 1993-02-11 1994-07-12 General Motors Corporation Fuel injector and check valve
US6752334B2 (en) 2001-07-13 2004-06-22 Siemens Diesel Systems Technology Fuel injector and method for controlling fuel flow
US8733673B2 (en) 2011-07-22 2014-05-27 Buescher Developments, LLP Electronic unit injector

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2616294A (en) * 1948-12-02 1952-11-04 Claude A Pickens Filtering liquid level gauge
DE937991C (en) * 1953-06-06 1956-01-19 Daimler Benz Ag Fuel tank
US2955787A (en) * 1956-12-27 1960-10-11 Lockheed Aircraft Corp Auxiliary fuel tank
US3001376A (en) * 1957-11-26 1961-09-26 British Oxygen Co Ltd Storage tanks for liquid oxygen and the like in rockets
US3396744A (en) * 1962-12-06 1968-08-13 Leo L. Schwarz System for elimination of condensation in fuel storage tanks
FR2398256A1 (en) * 1977-07-19 1979-02-16 Bayerische Motoren Werke Ag SUCTION STRAINER FOR THE SUCTION TUBING OF A LUBRICANT PUMP
US4655248A (en) * 1985-12-16 1987-04-07 United Technologies Corporation Check valve
US5020566A (en) * 1990-08-13 1991-06-04 Sullair Corporation Fuel supply system for portable engine driven equipment
US5328094A (en) * 1993-02-11 1994-07-12 General Motors Corporation Fuel injector and check valve
US6752334B2 (en) 2001-07-13 2004-06-22 Siemens Diesel Systems Technology Fuel injector and method for controlling fuel flow
US8733673B2 (en) 2011-07-22 2014-05-27 Buescher Developments, LLP Electronic unit injector

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