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US2683418A - Pump - Google Patents

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US2683418A
US2683418A US48613A US4861348A US2683418A US 2683418 A US2683418 A US 2683418A US 48613 A US48613 A US 48613A US 4861348 A US4861348 A US 4861348A US 2683418 A US2683418 A US 2683418A
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United States
Prior art keywords
pump
pressure
fluid
passage
valve
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Expired - Lifetime
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US48613A
Inventor
Jr Stanley B Smith
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Bendix Aviation Corp
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Bendix Aviation Corp
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Priority to US48613A priority Critical patent/US2683418A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • 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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/02Stopping, starting, unloading or idling control
    • F04B49/03Stopping, starting, unloading or idling control by means of valves
    • F04B49/035Bypassing
    • 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
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/13Special devices for making an explosive mixture; Fuel pumps
    • F02M2700/1317Fuel pumpo for internal combustion engines
    • 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
    • Y10T137/7781With separate connected fluid reactor surface
    • Y10T137/7793With opening bias [e.g., pressure regulator]
    • Y10T137/7809Reactor surface separated by apertured partition
    • Y10T137/782Reactor surface is diaphragm

Definitions

  • the present invention relates to pumps and more particularly to fluid pumps of the type having an automatic release or by-pass valve.
  • Another object of the invention is to provide in a pressure fuel system a pump means adapted to vary its delivery in accordance with the quantity of metered fuel supplied to the pump inlet.
  • Still another object of the invention is to provide a pump means of general utility adapted to so regulate the pump delivery that a substantially constant pressure or a predetermined variable pressure of the fluid is maintained at the pump inlet,
  • numera1 l9 designates generally a conventional positive displacement pump of the vane type, 12 a fluid inlet passageway for the pump, M a fluid outlet passage, It a fluid by-pass unit, said unit being connected to the pump outlet by the main fluid outlet conduit 63 and a branch conduit 20 and to the pump inlet by a conduit 22.
  • the pump H which may be of any other suitable type, such as for example a gear, centrifugal or reciprocating piston type pump, consists of a pump sleeve 24, a rotor 26 having, as shown in the drawing, four vanes 28 abutting against a floating pin 30 and contacting the internal surface of the sleeve, said rotor being adapted to revolve in the sleeve in a clockwise direction.
  • the fiuid is discharged from pump l8) through the main fluid conduit [8 and is divided at branch conduit 20 into two portions, one portion of the fluid continuing through the main discharge conduit l8 and the other portion flowing to the bypass unit and thence through conduit 22 to the pump inlet 12.
  • the fluid inlet of the by-pass unit is connected to conduit 2!] and thus to the pump inlet by passageways 4G and 42 disposed in a sleeve M in which a valve 48 is adapted toreciprocate and to seat over orifices 50 and 52 located at opposite ends of said sleeve. Since both the upper and lower ends of valve 48 are of substantially the same area and are subjected to substantially the same pressures, the operation of the valve is unaifected by variations in pressure in the by-pass unit.
  • Valve 53 is controlled by a flexible diaphragm I 68 subjected on one side to the pump inlet pressure transmitted through conduit 22, chamber 62 and a plurality of passages 64 to chamber 66 and on the other side to the force of a coil spring 68 calibrated and adjusted to maintain a predetermined 'pump inlet pressure, said spring reacting between the diaphragm and a spring retainer 12 on the end of an adjustment screw 16.
  • chamber 16 in which spring 68 is located is shown vented to the atmosphere through a port 78 however, for certain purposes it may be desirable to subject diaphragm to a variable pressure to obtain certain desired variations in the pump The inlet pressure, as will be more fully explained hereinafter.
  • the diagraphm and valve 45 are rigidly connected by a rod 88 threaded into the valve and locked in place by a nut 82.
  • the diaphragm at the marginal edge thereof is clamped between two sections of the unit housing and is given support in the. central portion by stiffening; bers 3d and 8t clamped to either side of the dia phragm between a shoulder 88 and a nut 95% on the upper end of rod 80.
  • the present pump and by-pass are especially adapted for use in a fuel metering. system wherein low fuel pressures for metering. are preferred but high pressures at a distributor or at the discharge nozzle are thereafter required.
  • the fuel pressure down stream from the metering orifice must be maintained at a substantially constant value while the upstream pressure and/or the effective size of the metering: orifice must be varied with variations in air flow to the engine.
  • the present in vention is adapted to maintain the downstream pressure. at a constant value. and at the same time provide a relatively high pressure for fuel delivery.
  • chamber “56 may be vented to some pressure other than atmospheric pressure.
  • chamber "l6 may be connected by a conduit with a venturi in the induction. passage of the engine so that on an increase in air flow to the engine, the pressure in chamber ill will become lower, causing diaphragm 8.53 to move in the valve closing direction. With the valve in a more nearly closed position, lessiuel is by-passed back to the pump inlet, thus resulting in a greater delivery of fuel to the engine and a slightly lower metered 4 fuel pressure at the inlet of the pump. With this condition prevailing, a greater diiierential across the metering orifice and thus a greater flow of fuel through the system are established for high power output.
  • the piunp may be any one of a number of well-known types provided the pump used is capable of delivering at all times a greater quantity of fluid than is delivered to the pump from the source of supply.
  • the pump and bypass may be constructed as an integral unit. Many other modifications may be made in the present pump and. by-pass to suit requirements.
  • a fluid pressure control device comprisin a fluid passage, a fluid pressure creating means in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow or" fluid therethrough, and a means actuated principally by variations in the. pressure in passage anterior to said pressure creating means for controlling said valve.
  • a fluid pressure control device comprising a fluid passage, a pump in said passage, a icy-- pass means having a conduit communicating with said passage anterior and posterior to said pump, a valve in said conduit for regulating the flow of fluid therethrough, said valve being substantially balanced against fluid pressure fluctu ations in the passage posterior to the pump, and a means actuated principally by variations in pressure at the inlet. passage of said pump for urging said valve toward closed position.
  • a fluid pressure control device comprising a fluid pressure creating means having a fluid inlet passage and a fluid outlet passage, a bypass means having a conduit communicating with said inlet passage and outlet passage, a valve in said conduit for regulating the flow of fluid therethrough, said valve being substantially balanced against pressure fluctuations in the fluid outlet-passage, and a diaphragm subjected on one side to a fluid pressure substantially equal to the pressure in said inlet passage for ccntrolling said valvein response to variations in said pressure.
  • a fluid pressure control device comprising a fluid passage, a fluid pressure creating means in said passage, a icy-passmeans having a conduit communicating: with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow of fluid. therethrough, said valve being substan tially balanced against pressure fluctuations in the passage posterior to said fluid pressure creating means, and a diaphragm subjected on one side to a fluid pressure substantially equal to the pressure in the passage anterior to said pressure creating means for urging said valve toward closed position.
  • a fluid pressure control device comprising a fluid passage, a pump in. said passage, a bypass means having a conduit communicating with said passage anterior and posterior to said pump, a substantially'balanced valve in said c011- duit for regulating the flow of fluid therethrough, a diaphragm subjected on. one side to a fluid pressure substantially equal to the pressure in said passage anterior to said pump for urging said valve toward closed position and on the other side to the force of resilient means for urging said valve toward open position.
  • a fluid pressure control device comprising a fluid passage, a fluid pressure creating means in said passage, a my-pass means having a conduit communicating with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow of fluid therethrough, and a diaphragm for controlling said valve responsive on one side to the pressure in said passage anterior to said pressure creating means for urging said valve toward closed position and on theother side to a variable fluid pressure.
  • a fluid pressure control device comprising a fluid passage, a pump in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pump, a valve in said conduit for regulating the flow of fluid therethrough, a diaphragm for controlling said valve responsive on one side to the pressure in said passage anterior to said pump for urging said valve toward closed position and on the other side to a variable fluid pressure and a spring for urging said valve toward open position.
  • a fluid pressure control device comprising a fluid passage, a pump in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pump, a

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Reciprocating Pumps (AREA)

Description

July 13, 1954 s. B. SMITH, JR
PUMP
Filed Sept. 19, 1948 1N VEN TOR. .STANLEYB. SMITH J2.
M M m p V m i W. 2 u @0 M 0 A 0 M ah i Z7 M 0 r W 5 0 6 w M.\ O. z L
Patented July 13, 1954 PUMP Stanley B. Smith, Jr., South Bend, Ind., assignor to Bendix Aviation Corporation, South Bend, Ind., a corporation of Delaware Application September 10, 1948, Serial No. 48,613
8 Claims.
The present invention relates to pumps and more particularly to fluid pumps of the type having an automatic release or by-pass valve.
In fuel supply systems for internal combustion engines and the like, it is usually desirable to meter the fuel at relatively low pressures in order to minimize line or joint failures and fuel leakage and permit the use of comparatively light sections in the several elements of the system. However, in fuel systems of the type in which the fuel is discharged directly into the combustion chamber of the cylinders or into the intake manifold adjacent the intake valves of the cylinders, it is necessary to discharge the fuel under high pressures which are much higher than normally desirable or feasible in fuel metering systems, in order to overcome the pressure in the cylinders for direct injection and to obtain good atomization of the fuel as it is discharged from the nozzle in either direct injection or manifold injection. It is, therefore, one of the principal objects of the present invention to provide in a low pressure fuel metering system a means for increasing the pressure of the metered fuel suificiently to overcome the high compression in the combustion chamber of the cylinders for direct injection of the fuel and to obtain good atomization of the fuel as it leaves the discharge nozzle in either direct injection or manifold injection.
Another object of the invention is to provide in a pressure fuel system a pump means adapted to vary its delivery in accordance with the quantity of metered fuel supplied to the pump inlet.
Still another object of the invention is to provide a pump means of general utility adapted to so regulate the pump delivery that a substantially constant pressure or a predetermined variable pressure of the fluid is maintained at the pump inlet,
Further objects and advantages of the invention will become apparent from the following description with reference to the accompanying drawing, wherein one specific embodiment of my pump means is shown schematically. From the detailed description which follows, modifications of and additions to the present invention will become apparent to those skilled in the art, and it is to be understood that although only one embodiment of the invention is disclosed in detail, many variations employing the fundamental features of the invention are possible and it is contemplated to use any such variations in structure, arrangement and mode of operation that may properly fall within the scope of the invention.
The invention in its broadest aspect includes a fluid passage, a pressure creating means for receiving fluid from a source, and for delivering the fluid through the passage at a substantially increased pressure and a by-pass around said means so constructed and arranged as to maintain a constant or otherwise predetermined inlet pressure for said means irrespective of the quantity of fluid supplied thereto. Referring specifically to the drawing, numera1 l9 designates generally a conventional positive displacement pump of the vane type, 12 a fluid inlet passageway for the pump, M a fluid outlet passage, It a fluid by-pass unit, said unit being connected to the pump outlet by the main fluid outlet conduit 63 and a branch conduit 20 and to the pump inlet by a conduit 22. The pump H], which may be of any other suitable type, such as for example a gear, centrifugal or reciprocating piston type pump, consists of a pump sleeve 24, a rotor 26 having, as shown in the drawing, four vanes 28 abutting against a floating pin 30 and contacting the internal surface of the sleeve, said rotor being adapted to revolve in the sleeve in a clockwise direction.
The fiuid is discharged from pump l8) through the main fluid conduit [8 and is divided at branch conduit 20 into two portions, one portion of the fluid continuing through the main discharge conduit l8 and the other portion flowing to the bypass unit and thence through conduit 22 to the pump inlet 12. The fluid inlet of the by-pass unit is connected to conduit 2!] and thus to the pump inlet by passageways 4G and 42 disposed in a sleeve M in which a valve 48 is adapted toreciprocate and to seat over orifices 50 and 52 located at opposite ends of said sleeve. Since both the upper and lower ends of valve 48 are of substantially the same area and are subjected to substantially the same pressures, the operation of the valve is unaifected by variations in pressure in the by-pass unit.
Valve 53 is controlled by a flexible diaphragm I 68 subjected on one side to the pump inlet pressure transmitted through conduit 22, chamber 62 and a plurality of passages 64 to chamber 66 and on the other side to the force of a coil spring 68 calibrated and adjusted to maintain a predetermined 'pump inlet pressure, said spring reacting between the diaphragm and a spring retainer 12 on the end of an adjustment screw 16. chamber 16 in which spring 68 is located is shown vented to the atmosphere through a port 78 however, for certain purposes it may be desirable to subject diaphragm to a variable pressure to obtain certain desired variations in the pump The inlet pressure, as will be more fully explained hereinafter.
The diagraphm and valve 45 are rigidly connected by a rod 88 threaded into the valve and locked in place by a nut 82. The diaphragm at the marginal edge thereof is clamped between two sections of the unit housing and is given support in the. central portion by stiffening; bers 3d and 8t clamped to either side of the dia phragm between a shoulder 88 and a nut 95% on the upper end of rod 80.
In the operation of the present pump and bypass unit, with the inlet pressure initially at a predetermined value, fluid is. pumped continuously from inlet !2 through conduit iii, a portion of said fluid being by-passed back. through unit it to the pump inlet and the remainder continuing on through conduit 13. If, during the oper ation, the quantity of fluid supplied to the pump diminishes, the pressure at the pump inlet decreases. The, lower pressure thus created is transmitted through conduit 26,, chamber 62, conduits 8 to chamber 6.6. adjacent. diaphragm (it which moves downwardly,. as shown in the drawing, in the valve opening direction so that sufficient fluid is returned. to the inlet side of the pump to re-establish the ori inal predetermined pressure at the inlet. If, on the other hand, there is an increase in the quantity of fluidsup plied to the inlet of. apump, a temporary rise in the fluid inlet pressure. results. This increased pressure is. transmitted to chamber 66 adjacent diaphragm to which moves upwardly in the valve closing directionso that a smaller quantity of fluid. is by-passed. back to the pump inlet and a greater quantity is delivered through the main discharge conduit 58- and the original predetermined pressure is rte-established. Itis thus seen that, regardless of the quantity of fluid supplied to the pump, the pump. and by-pass unit operate to maintain a constant or otherwise predetermined pressure of the fluid at the inlet of the pump.
The present pump and by-pass are especially adapted for use in a fuel metering. system wherein low fuel pressures for metering. are preferred but high pressures at a distributor or at the discharge nozzle are thereafter required. In some fuel metering systems, the fuel pressure down stream from the metering orifice must be maintained at a substantially constant value while the upstream pressure and/or the effective size of the metering: orifice must be varied with variations in air flow to the engine. The present in vention is adapted to maintain the downstream pressure. at a constant value. and at the same time provide a relatively high pressure for fuel delivery. A fuel metering system incorporat ing the foregoing features is disclosed and.
claimed. in my copending application Serial No; 49,967 flled on September 18, 1948, now Patent No. 2,633,187.
As previously pointed out herein, chamber "56 may be vented to some pressure other than atmospheric pressure. For. example, in a fuel system for an internal combustion engine, chamber "l6 may be connected by a conduit with a venturi in the induction. passage of the engine so that on an increase in air flow to the engine, the pressure in chamber ill will become lower, causing diaphragm 8.53 to move in the valve closing direction. With the valve in a more nearly closed position, lessiuel is by-passed back to the pump inlet, thus resulting in a greater delivery of fuel to the engine and a slightly lower metered 4 fuel pressure at the inlet of the pump. With this condition prevailing, a greater diiierential across the metering orifice and thus a greater flow of fuel through the system are established for high power output.
Various modifications and arrangements may be made in the present pump and by-pass. For example, the piunp may be any one of a number of well-known types provided the pump used is capable of delivering at all times a greater quantity of fluid than is delivered to the pump from the source of supply. Further, the pump and bypass may be constructed as an integral unit. Many other modifications may be made in the present pump and. by-pass to suit requirements.
1'.- claim:
1. A fluid pressure control device comprisin a fluid passage, a fluid pressure creating means in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow or" fluid therethrough, and a means actuated principally by variations in the. pressure in passage anterior to said pressure creating means for controlling said valve.
A fluid pressure control device comprising a fluid passage, a pump in said passage, a icy-- pass means having a conduit communicating with said passage anterior and posterior to said pump, a valve in said conduit for regulating the flow of fluid therethrough, said valve being substantially balanced against fluid pressure fluctu ations in the passage posterior to the pump, and a means actuated principally by variations in pressure at the inlet. passage of said pump for urging said valve toward closed position.
3. A fluid pressure control device comprising a fluid pressure creating means having a fluid inlet passage and a fluid outlet passage, a bypass means having a conduit communicating with said inlet passage and outlet passage, a valve in said conduit for regulating the flow of fluid therethrough, said valve being substantially balanced against pressure fluctuations in the fluid outlet-passage, and a diaphragm subjected on one side to a fluid pressure substantially equal to the pressure in said inlet passage for ccntrolling said valvein response to variations in said pressure.
4. A fluid pressure control device comprising a fluid passage, a fluid pressure creating means in said passage, a icy-passmeans having a conduit communicating: with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow of fluid. therethrough, said valve being substan tially balanced against pressure fluctuations in the passage posterior to said fluid pressure creating means, and a diaphragm subjected on one side to a fluid pressure substantially equal to the pressure in the passage anterior to said pressure creating means for urging said valve toward closed position.
5. A fluid pressure control device comprising a fluid passage, a pump in. said passage, a bypass means having a conduit communicating with said passage anterior and posterior to said pump, a substantially'balanced valve in said c011- duit for regulating the flow of fluid therethrough, a diaphragm subjected on. one side to a fluid pressure substantially equal to the pressure in said passage anterior to said pump for urging said valve toward closed position and on the other side to the force of resilient means for urging said valve toward open position.
6. A fluid pressure control device comprising a fluid passage, a fluid pressure creating means in said passage, a my-pass means having a conduit communicating with said passage anterior and posterior to said pressure creating means, a valve in said conduit for regulating the flow of fluid therethrough, and a diaphragm for controlling said valve responsive on one side to the pressure in said passage anterior to said pressure creating means for urging said valve toward closed position and on theother side to a variable fluid pressure.
7. A fluid pressure control device comprising a fluid passage, a pump in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pump, a valve in said conduit for regulating the flow of fluid therethrough, a diaphragm for controlling said valve responsive on one side to the pressure in said passage anterior to said pump for urging said valve toward closed position and on the other side to a variable fluid pressure and a spring for urging said valve toward open position.
6 8. A fluid pressure control device comprising a fluid passage, a pump in said passage, a by-pass means having a conduit communicating with said passage anterior and posterior to said pump, a
References Cited in the file Of this patent UNITED STATES PATENTS Number Name Date 1,935,544 Delancey Nov. 14, 1933 2,170,530 Johnson Aug. 22, 1939 2,294,609 Schlosser Sept. 1, 1942 2,299,079 Davis Oct. 20, 1942 2,368,883 Roth Feb. 6, 1945 2,406,973 Trisler Sept. 3, 1946 2,409,975 Curtis Oct. 22, 1946 2,411,574 Hunt Nov. 26, 1946
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Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2821140A (en) * 1954-01-28 1958-01-28 Vickers Inc Power transmission
DE1033366B (en) * 1954-06-15 1958-07-03 Leybolds Nachfolger E Pump combination with high suction power
US2943575A (en) * 1954-01-28 1960-07-05 Vickers Inc Power transmission
US3021790A (en) * 1958-05-23 1962-02-20 Blackmer Pump Company Pump delivery control mechanism
US3056259A (en) * 1957-01-28 1962-10-02 Rolls Royce Engine liquid fuel supply system
US3103891A (en) * 1959-10-01 1963-09-17 Roper Hydraulics Inc Unloading relief valve
US3125028A (en) * 1964-03-17 rohde
US3183839A (en) * 1965-05-18 Pump control
US3233651A (en) * 1962-05-28 1966-02-08 Holley Carburetor Co Fluid metering system
US3266426A (en) * 1964-02-20 1966-08-16 Dover Corp Pump control
US4060343A (en) * 1976-02-19 1977-11-29 Borg-Warner Corporation Capacity control for rotary compressor
US4170204A (en) * 1976-09-30 1979-10-09 Audi Nsu Auto Union Aktiengesellschaft Fuel injection system
US4205637A (en) * 1976-12-13 1980-06-03 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic fuel injection system for an internal combustion engine having electromagnetic valves and a fuel damper upstream thereof
US4222712A (en) * 1978-02-15 1980-09-16 Sundstrand Corporation Multiple displacement pump system with bypass controlled by inlet pressure
US4392347A (en) * 1981-07-27 1983-07-12 General Motors Corporation Gas turbine engine fuel system
US4505647A (en) * 1978-01-26 1985-03-19 Grumman Allied Industries, Inc. Vacuum pumping system
US4531359A (en) * 1983-11-04 1985-07-30 General Motors Corporation Gas turbine engine fuel system
US4886425A (en) * 1987-03-26 1989-12-12 Mitsubishi Jukogyo Kabushiki Kaisha Capacity control device of scroll-type fluid compressor
US5292234A (en) * 1993-05-03 1994-03-08 Ford Motor Company System for preventing cavitation in an hydraulic pump
US5333999A (en) * 1992-03-12 1994-08-02 Aisin Seiki Kabushiki Kaisha Variable displacement compressor
EP2282213A1 (en) * 2009-08-04 2011-02-09 F. Hoffmann-La Roche AG Sample preparation dosing unit

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1935544A (en) * 1932-01-14 1933-11-14 Gilbert & Barker Mfg Co Liquid dispensing pump
US2170530A (en) * 1937-10-25 1939-08-22 Pump Engineering Service Corp Fuel pump
US2294609A (en) * 1940-10-21 1942-09-01 Candler Hill Corp Pump
US2299079A (en) * 1939-09-15 1942-10-20 Walwin L Davis Relief valve
US2368883A (en) * 1942-12-12 1945-02-06 Pesco Products Co Multiple discharge pump
US2406973A (en) * 1942-11-27 1946-09-03 Gen Motors Corp Altitude compensator for fuel pumps
US2409975A (en) * 1943-03-06 1946-10-22 Curtis Pump Co Pump pressure control system
US2411574A (en) * 1944-03-06 1946-11-26 Chandler Evans Corp Pump control with line loss compensation

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1935544A (en) * 1932-01-14 1933-11-14 Gilbert & Barker Mfg Co Liquid dispensing pump
US2170530A (en) * 1937-10-25 1939-08-22 Pump Engineering Service Corp Fuel pump
US2299079A (en) * 1939-09-15 1942-10-20 Walwin L Davis Relief valve
US2294609A (en) * 1940-10-21 1942-09-01 Candler Hill Corp Pump
US2406973A (en) * 1942-11-27 1946-09-03 Gen Motors Corp Altitude compensator for fuel pumps
US2368883A (en) * 1942-12-12 1945-02-06 Pesco Products Co Multiple discharge pump
US2409975A (en) * 1943-03-06 1946-10-22 Curtis Pump Co Pump pressure control system
US2411574A (en) * 1944-03-06 1946-11-26 Chandler Evans Corp Pump control with line loss compensation

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125028A (en) * 1964-03-17 rohde
US3183839A (en) * 1965-05-18 Pump control
US2821140A (en) * 1954-01-28 1958-01-28 Vickers Inc Power transmission
US2943575A (en) * 1954-01-28 1960-07-05 Vickers Inc Power transmission
DE1033366B (en) * 1954-06-15 1958-07-03 Leybolds Nachfolger E Pump combination with high suction power
US3056259A (en) * 1957-01-28 1962-10-02 Rolls Royce Engine liquid fuel supply system
US3021790A (en) * 1958-05-23 1962-02-20 Blackmer Pump Company Pump delivery control mechanism
US3103891A (en) * 1959-10-01 1963-09-17 Roper Hydraulics Inc Unloading relief valve
US3233651A (en) * 1962-05-28 1966-02-08 Holley Carburetor Co Fluid metering system
US3266426A (en) * 1964-02-20 1966-08-16 Dover Corp Pump control
US4060343A (en) * 1976-02-19 1977-11-29 Borg-Warner Corporation Capacity control for rotary compressor
US4170204A (en) * 1976-09-30 1979-10-09 Audi Nsu Auto Union Aktiengesellschaft Fuel injection system
US4205637A (en) * 1976-12-13 1980-06-03 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic fuel injection system for an internal combustion engine having electromagnetic valves and a fuel damper upstream thereof
US4505647A (en) * 1978-01-26 1985-03-19 Grumman Allied Industries, Inc. Vacuum pumping system
US4222712A (en) * 1978-02-15 1980-09-16 Sundstrand Corporation Multiple displacement pump system with bypass controlled by inlet pressure
US4392347A (en) * 1981-07-27 1983-07-12 General Motors Corporation Gas turbine engine fuel system
US4531359A (en) * 1983-11-04 1985-07-30 General Motors Corporation Gas turbine engine fuel system
US4886425A (en) * 1987-03-26 1989-12-12 Mitsubishi Jukogyo Kabushiki Kaisha Capacity control device of scroll-type fluid compressor
US5333999A (en) * 1992-03-12 1994-08-02 Aisin Seiki Kabushiki Kaisha Variable displacement compressor
US5292234A (en) * 1993-05-03 1994-03-08 Ford Motor Company System for preventing cavitation in an hydraulic pump
EP2282213A1 (en) * 2009-08-04 2011-02-09 F. Hoffmann-La Roche AG Sample preparation dosing unit
US20110030803A1 (en) * 2009-08-04 2011-02-10 Roche Diagnostics Operations, Inc. Sample Preparation Dosing Unit
US8778281B2 (en) 2009-08-04 2014-07-15 Roche Diagnostics Operations, Inc Sample preparation dosing unit

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