US3856436A - Power transmission - Google Patents

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Publication number
US3856436A
US3856436A US00315945A US31594572A US3856436A US 3856436 A US3856436 A US 3856436A US 00315945 A US00315945 A US 00315945A US 31594572 A US31594572 A US 31594572A US 3856436 A US3856436 A US 3856436A
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United States
Prior art keywords
restrictor
pump
pressure
pilot
adjustable orifice
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
US00315945A
Inventor
K Lonnemo
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Vickers Inc
Original Assignee
Sperry Rand 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 Sperry Rand Corp filed Critical Sperry Rand Corp
Priority to US00315945A priority Critical patent/US3856436A/en
Priority to AU60289/73A priority patent/AU473650B2/en
Priority to CA180,910A priority patent/CA983314A/en
Priority to IT52924/73A priority patent/IT996264B/en
Priority to DE19732350390 priority patent/DE2350390A1/en
Priority to FR7338681A priority patent/FR2211054A5/fr
Priority to JP48127638A priority patent/JPS589276B2/en
Priority to GB5706473A priority patent/GB1383490A/en
Priority to SE7317029A priority patent/SE383190B/en
Application granted granted Critical
Publication of US3856436A publication Critical patent/US3856436A/en
Assigned to SPERRY CORPORATION reassignment SPERRY CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SPERRY RAND CORPORATION
Assigned to VICKERS, INCORPORATED reassignment VICKERS, INCORPORATED ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: SPERRY CORPORATION A DE CORP.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • 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
    • F04B49/08Regulating by delivery pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B2205/00Fluid parameters
    • F04B2205/08Pressure difference over a throttle

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Reciprocating Pumps (AREA)
  • Control Of Positive-Displacement Pumps (AREA)
  • Control Of Fluid Gearings (AREA)

Abstract

A pilot operated load compensated variable displacement pump is controlled by a servomotor and a pilot valve to maintain a constant pressure drop across an adjustable orifice in the pump delivery line. The available pressure differential for operating the pilot valve is increased without increasing the pressure drop in the main flow through the adjustable orifice by providing a small restrictor in the operating line to the pilot valve and establishing a continuous bleed flow through that restrictor to establish a large pressure differential supplementing that at the adjustable orifice in the main pump delivery line. The bleed is established through a pressure compensated flow control valve. Maximum pressure limiting is obtained by a pilot relief valve establishing a parallel bleed. Alternatively, a special pilot relief valve establishes both the bleed flow and the maximum pressure limiting.

Description

United States Patent 1191 Lonnemo 1451 Dec. 24, 1974 [73] Assignee: Sperry Rand Corporation, Troy,
Mich.
221 Filed: Dec. 18,1972
21 Appl. N6; 315,945
Primary ExaminerWilliam L. Freeh Assistant Examiner-Gregg Paul LaPointe Attorney, Agent, or Firm-Theodore Van Meter [57] ABSTRACT A pilot operated load compensated variable displacement pump is controlled by a servomotor and a pilot valve to maintain a constant pressure drop across an [52] US Cl. 417/212, 60/450 adjustable orifice in the pump delivery line. The avail- [51] Int. Cl. F04b 1/00 able pressure differential for operating the pilot valve [58] Field of Search 417/213, 218, 220, 221, is increased without increasing the pressure drop in 417/222; 91/506; 60/450 the main flow through the adjustable orifice by providing a small restrictor in the operating line to the pilot [56] References Cited valve and establishing a continuous bleed flow through IT STATES PATENTS that restrictor to establish a large pressure differential 2 255 783 9H9 Kendrick 60,450 supplementing that at the adjustable orifice in the 3 6/1959 Van 60/450 main pump delivery line. The bleed is established 3,067,693 12/1962 Lambeck 1. 417/219 through a Pressure Compensated flow control valve- 3,188,971 6/1965 Puryear 417/222 Maximum pressure limiting is obtained by a pilot relief 3,246,471 4/1966 Goodale 60/450 valve establishing a parallel bleed. Alternatively, a 3,444,689 5/1969 Budzich 60/450 special pilot relief valve establishes both the bleed McMillen CI al. flow and the maximum pressure 3,644,063 2/1972 Bosch 417/213 3,768,928 10/1973 Miller et a1. 417 213 4 Claims, 2 Drawlng Flgul'es LL 5 l8/- L l Z0 POWER TRANSMISSION Conventional load compensated variable displacement pumps have a displacement regulator which is governed by the pressure drop across one or more adjustable orifices in the pump delivery line, thus, automatically regulating the pump delivery to the volumetric flow requirements determined by the size of the adjustable orifice, or orifices. Customarily, such an orifice is found in the variable opening of the usual main directional valve controlling flow to a fluid motor. In such systems, the regulator requires a substantial pressure available for its operation and this is determined by the amount of pressure drop across the adjustable orifice. Thus, if reasonable dynamic behavior is to be had at the regulator, a very substantial pressure drop is imposed upon all of the fluid flowing through the adjustable orifice or directional valve. In systems which transmit large amounts of power hydraulically, this represents a substantial loss through throttling.
The present invention aims to provide an improved load compensated variable displacement pump in which the available pressure for operating the regulator is high, while the pressure drop through the adjustable orifice in the main delivery line is a low one, and thus throttling losses in the main power flow are minimized.
This is achieved by the provision of a pilot operated, load compensated, variable displacement pump for maintaining a predetermined pressure drop across an adjustable orifice which comprises a servomotor for adjusting the pump displacement, a pilot valve for controlling the servomotor, a connection from the pump output ahead of the adjustable orifice for urging the pilot valve toward a position of lesser pump displacement, a connection from the pump output beyond the adjustable orifice for urging the pilot valve toward a position of greater pump displacement, a restrictor in the second connection, and a bleed restriction from the restrictor to maintain a small continuous flow therethrough sufficient to create a pressure drop through the restrictor several times as great as the pressure drop through the adjustable orifice under steady state conditions, whereby a large pressure differential for operating the pilot valve is available without imposing a large pressure drop in the main flow through the adjustable orifice.
In the drawing:
FIG. 1 represents a hydraulic circuit diagram of a pump and control system incorporating a preferred form of the present invention.
FIG. 2 represents a modified form of the present invention.
A variable displacement pump has a servomotor 12 for adjusting its displacement and feeds its output into a delivery line 14. The delivery line 14 leads through an adjustable orifice 16 to a fluid utilization device 18. The adjustable orifice 16 is representative of many types of valves which control the rate of flow to the fluid utilization device, such as one or more fluid motors. In many systems, of which this is typical, the adjustable orifice 16 may comprise a conventional four-way reverse valve.
The servomotor 12 is controlled by a three-way pilot valve 20 which can supply fluid to the servomotor 12 from the supply line through a branch 22 or can exhaust fluid from the servomotor through an exhaust line 24. The pilot valve 20 is urged to the left against a spring 26 by delivery line pressure directed through a brnach 28. Also acting on the pilot valve 20 in opposition to delivery line pressure is a lower pressure derived from the delivery line after passing through the adjustable orifice 16 and a fixed orifice 30. This pressure is transmitted through a branch 32. A continuous bleed flow through the'restrictor 30 is established by a branch 34 containing a pressure compensated flow control valve 36 feeding into the exhaust line 24. For the purpose of establishing a maximum pressure limit in the system, a pilot relief valve 38 is connected as an additional possible bleed from the orifice 30 through a branch 40.
In operation, with the pumplO running and with the servomotor 12 stationary because of the pilot valve 20 being in the neutral position, the pump outlet pressure in lines 14, 22 and 28, transmitted to the right end of pilot valve 20, is exactly balanced by the force of spring 26 and the pressure maintained in line 32 on the left end of pilot valve 20. This pressure is determined by the sum of the pressure drops through the adjustable orifice l6 and the restrictor 30. The pressure drop at restrictor 30 is determined by the setting of the flow control valve 36 which determines the fixed and continuous bleed flow through the restrictor 30.
When the adjustable orifice 16 is changed to a more restricted position, for example, this causes a temporary pressure rise in conduits 14, 22 and 28 which shifts the pilot valve 20 to the left admitting pressure fluid to the servomotor l2 and reducing the pump displacement. Motion of the valve 20 to the left pumps a small quantity of fluid upwardly through line 32 into the bleed circuit thus reducing the flow rate through restrictor 30 and consequently reducing the pressure at its outlet. When the pump displacement has been reduced to the value necessary to maintain the previous pressure drop through the adjustable orifice 16, the valve 20 will return to its neutral position. A similar but opposite action occurs upon an opening adjustment of orifice 16. Whenever the system pressure rises above a predetermined limit, the pilot relief valve 38 will open, causing a further bleed flow through the orifice 30, thus dropping the pressure in conduit 32 and allowing pilot valve 20 to shift to the left and reduce the pump displacement until the pressure overload has ceased.
The pressure available for operating pilot valve 20 is theoretically the sum of the pressure drops through adjustable orifice 16 and restrictor 30. By making the latter pressure drop relatively high, say five times as high as the former pressure drop, it will be seen that effective control of the pilot valve 20 is maintained without imposing a large pressure drop through the adjustable orifice 16. In this way, substantial power losses in the main flow line are avoided.
In the modification illustrated in FIG. 2, a special pilot relief valve 42 is provided to take the place of the flow control valve 36 and the pilot relief valve 38 together. Thus the inner spring 44 of the relief valve poppet is adjusted automatically by means of a piston 46 having a diameter equal to the seat diameter of the poppet. A head 48 limits the stroke of piston 46 and a branch line 50 connects the piston 46 to a point ahead of the restrictor 30. An auxiliary spring 52 aids in biasing the piston 46 against this pressure.
Thus, depending upon the pressure drop across the restrictor 30, the piston 46 will take up a certain position balancing this pressure drop against the force of springs 44 and 52 and will vary the pressure setting of the pilot relief valve 42 correspondingly. A continuous quiescent flow is accordingly maintained through restrictor 30 which is at a substantially constant rate because of the constant pressure drop across restrictor 30.
I claim:
1. A pilot operated load compensated variable displacement pump for maintaining a predetermined pressure drop across an adjustable orifice comprising a servomotor for adjusting the pump displacement, a pilot valve for controlling the servomotor, a connection from the pump output ahead of the adjustable orifice for urging the pilot valve toward a position of lesser pump displacement, a second connection from the pump output beyond the adjustable orifice for urging the pilot valve toward a position of greater displacement, a restrictor in the second connection and a bleed restriction comprising a pressure responsive flow regulator from the restrictor to maintain a small and fixed continuous flow therethrough independent of system pressure and sufficient to create a pressure drop through the restrictor several times as great as the pressure drop through the adjustable orifice under steady state conditions, whereby a large pressure differential for operating the pilot valve is available without imposing a large pressure drop in the main flow through the adjustable orifice.
2. A pump as defined in claim 1 wherein the flow regulator comprises an additional restrictor and a compensator for maintaining a constant pressure drop across the additional restrictor.
3. A pump as defined in claim 1 which includes a pilot relief valve connected to the restrictor to limit the maximum pump output pressure.
4. A pump as defined in claim 2 having a pilot relief valve connected to the first restrictor to limit the maxi mum pump output pressure.

Claims (4)

1. A pilot operated load compensated variable displacement pump for maintaining a predetermined pressure drop across an adjustable orifice comprising a servomotor for adjusting the pump displacement, a pilot valve for controlling the servomotor, a connection from the pump output ahead of the adjustable orifice for urging the pilot valve toward a position of lesser pump displacement, a second connection from the pump output beyond the adjustable orifice for urging the pilot valve toward a position of greater displacement, a restrictor in the second connection and a bleed restriction comprising a pressure responsive flow regulator from the restrictor to maintain a small and fixed continuous flow therethrough independent of system pressure and sufficient to create a pressure drop through the restrictor several times as great as the pressure drop through the adjustable orifice under steady state conditions, whereby a large pressure differential for operating the pilot valve is available without imposing a large pressure drop in the main flow through the adjustable orifice.
2. A pump as defined in claim 1 wherein the flow regulator comprises an additional restrictor and a compensator for maintaining a constant pressure drop across the additional restrictor.
3. A pump as defined in claim 1 which includes a pilot relief valve connected to the restrictor to limit the maximum pump output pressure.
4. A pump as defined in claim 2 having a pilot relief valve connected to the first restrictor to limit the maximum pump output pressure.
US00315945A 1972-12-18 1972-12-18 Power transmission Expired - Lifetime US3856436A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
US00315945A US3856436A (en) 1972-12-18 1972-12-18 Power transmission
AU60289/73A AU473650B2 (en) 1972-12-18 1973-09-13 Pilot operated load compensated variable displacement pump
CA180,910A CA983314A (en) 1972-12-18 1973-09-13 Variable displacement hydraulic pump
IT52924/73A IT996264B (en) 1972-12-18 1973-10-04 IMPROVEMENT IN VARIABLE FLOW PUMP ARRANGEMENTS FOR HYDRAULIC SYSTEMS
DE19732350390 DE2350390A1 (en) 1972-12-18 1973-10-08 LOAD COMPENSATED PUMP WITH VARIABLE DISPLACEMENT
FR7338681A FR2211054A5 (en) 1972-12-18 1973-10-30
JP48127638A JPS589276B2 (en) 1972-12-18 1973-11-13 Pilot operated load compensated variable displacement pump
GB5706473A GB1383490A (en) 1972-12-18 1973-12-10 Pumps
SE7317029A SE383190B (en) 1972-12-18 1973-12-17 LOAD COMPENSATED PUMP WITH VARIABLE DEPLACEMENT.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00315945A US3856436A (en) 1972-12-18 1972-12-18 Power transmission

Publications (1)

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US3856436A true US3856436A (en) 1974-12-24

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US00315945A Expired - Lifetime US3856436A (en) 1972-12-18 1972-12-18 Power transmission

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Country Link
US (1) US3856436A (en)
JP (1) JPS589276B2 (en)
AU (1) AU473650B2 (en)
CA (1) CA983314A (en)
DE (1) DE2350390A1 (en)
FR (1) FR2211054A5 (en)
GB (1) GB1383490A (en)
IT (1) IT996264B (en)
SE (1) SE383190B (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS525864A (en) * 1975-06-28 1977-01-17 Hehl Karl Controlling system for hydraulic pressure circuit of injection molder
US4067664A (en) * 1974-12-31 1978-01-10 Robert Bosch Gmbh Control system for a pump
US4118149A (en) * 1976-02-05 1978-10-03 Hytec Ab Output regulation in hydraulic and hydropneumatic systems
US4123202A (en) * 1975-11-04 1978-10-31 Plessey Handel Und Investments Ag Hydraulic pumping arrangements
US4194364A (en) * 1977-05-21 1980-03-25 Robert Bosch Gmbh Arrangement for controlling the operation of a fluid-displacement machine
US4194363A (en) * 1979-02-21 1980-03-25 General Signal Corporation Fluid horsepower control system
JPS5554701A (en) * 1978-09-28 1980-04-22 Eaton Corp Loaddresponsible controller for hydraulic system
US4292805A (en) * 1979-09-24 1981-10-06 Rexnord Inc. Servo-valve convertible construction
JPS61204002U (en) * 1986-05-14 1986-12-22
JPS62801U (en) * 1986-05-14 1987-01-07
US4976106A (en) * 1988-02-18 1990-12-11 Linde Aktiengesellschaft Load-sensing variable displacement pump controller with adjustable pressure-compensated flow control valve in feedback path
US5203678A (en) * 1990-01-11 1993-04-20 Hitachi Construction Machinery Co., Ltd. Valve apparatus and hydraulic drive system
US5319932A (en) * 1993-04-28 1994-06-14 Roche Engineering Corporation Power sensing regenerator
GB2279776A (en) * 1993-05-28 1995-01-11 Dana Corp A hydraulic load sensing system
EP0869285A3 (en) * 1997-04-04 1999-09-22 Brueninghaus Hydromatik Gmbh Load sensing control with flushing circuit
US20050047930A1 (en) * 2002-03-06 2005-03-03 Johannes Schmid System for controlling a hydraulic variable-displacement pump
CN103982475A (en) * 2014-05-30 2014-08-13 湖南五新重型装备有限公司 Hydraulic control system for concrete spraying vehicle boom frame
US20160003237A1 (en) * 2013-03-27 2016-01-07 Kayaba Industry Co., Ltd. Pump discharge flow-rate control device

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3941513A (en) * 1974-09-05 1976-03-02 Parker-Hannifin Corporation Variable displacement pump control assembly
US4017219A (en) * 1975-12-22 1977-04-12 Abex Corporation Control system for variable displacement pumps
US4029439A (en) * 1975-12-22 1977-06-14 Abex Corporation Control system for variable displacement pumps
DE2840687A1 (en) * 1978-09-19 1980-04-03 Bosch Gmbh Robert DEVICE FOR CONTROLLING THE FLOW RATE AND LIMITING THE DELIVERY PRESSURE OF AN ADJUSTABLE PUMP.
DE2906166A1 (en) * 1979-02-17 1980-08-28 Bosch Gmbh Robert DEVICE FOR CONTROLLING THE FLOW RATE AND LIMITING THE DELIVERY PRESSURE OF AN ADJUSTABLE PUMP
DE3016609A1 (en) * 1980-04-30 1981-11-05 G.L. Rexroth Gmbh, 8770 Lohr Radial vane type pump - has throughput controlled by positioning valve energised by signal from discharge flow meter
DE3027819A1 (en) * 1980-07-23 1982-02-25 Backe, Wolfgang, Prof.Dr.-Ing., 5100 Aachen DEVICE FOR REGULATING A VARIABLE PUMP
DE3044143A1 (en) * 1980-11-24 1982-06-24 Linde Ag, 6200 Wiesbaden CONTROL DEVICE FOR A HYDROSTATIC DRIVE SYSTEM
DE3146513A1 (en) * 1980-11-24 1982-06-24 Linde Ag, 6200 Wiesbaden Control device for a hydrostatic drive system
DE3112561C2 (en) * 1981-03-30 1985-09-26 Danfoss A/S, Nordborg Control device for a liquid pump with adjustable delivery volume
DE3129440A1 (en) * 1981-07-25 1983-02-10 Mannesmann Rexroth GmbH, 8770 Lohr Control device for a variable-delivery pump
DE3211307A1 (en) * 1982-03-26 1983-09-29 Linde Ag, 6200 Wiesbaden ADJUSTABLE AXIAL PISTON PUMP WITH A CONTROL ORGAN AND CONTROLLER FOR SUCH
DE8335902U1 (en) * 1983-12-14 1987-06-04 Brueninghaus Hydraulik Gmbh, 7240 Horb, De
DE3622939A1 (en) * 1986-07-08 1988-01-14 Linde Ag Hydraulic control or regulating device
DE3844398C2 (en) * 1988-12-30 1997-07-31 Rexroth Mannesmann Gmbh Hydraulic circuit for a variable pump
DE8906826U1 (en) * 1989-06-03 1989-09-07 Keicher, Siegfried, 7906 Blaustein, De
DE4025638C1 (en) * 1990-08-13 1991-12-05 Brueninghaus Hydraulik Gmbh, 7240 Horb, De
DE4337210A1 (en) * 1993-10-30 1995-05-04 Rexroth Mannesmann Gmbh Central hydraulic installation for a motor vehicle

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US2255783A (en) * 1940-02-17 1941-09-16 Manly Corp Fluid pressure device and system
US2892311A (en) * 1958-01-08 1959-06-30 Deere & Co Hydraulic apparatus
US3067693A (en) * 1958-12-24 1962-12-11 United Aircraft Corp Control means for variable delivery pump
US3188971A (en) * 1962-08-13 1965-06-15 Bendix Corp Control system for a pump
US3246471A (en) * 1964-12-10 1966-04-19 Ford Motor Co Hydraulic drive control
US3444689A (en) * 1967-02-02 1969-05-20 Weatherhead Co Differential pressure compensator control
US3635021A (en) * 1969-10-16 1972-01-18 Borg Warner Hydraulic system
US3644063A (en) * 1969-04-05 1972-02-22 Bosch Gmbh Robert Regulated hydraulic apparatus
US3768928A (en) * 1971-06-01 1973-10-30 Borg Warner Pump control system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2255783A (en) * 1940-02-17 1941-09-16 Manly Corp Fluid pressure device and system
US2892311A (en) * 1958-01-08 1959-06-30 Deere & Co Hydraulic apparatus
US3067693A (en) * 1958-12-24 1962-12-11 United Aircraft Corp Control means for variable delivery pump
US3188971A (en) * 1962-08-13 1965-06-15 Bendix Corp Control system for a pump
US3246471A (en) * 1964-12-10 1966-04-19 Ford Motor Co Hydraulic drive control
US3444689A (en) * 1967-02-02 1969-05-20 Weatherhead Co Differential pressure compensator control
US3644063A (en) * 1969-04-05 1972-02-22 Bosch Gmbh Robert Regulated hydraulic apparatus
US3635021A (en) * 1969-10-16 1972-01-18 Borg Warner Hydraulic system
US3768928A (en) * 1971-06-01 1973-10-30 Borg Warner Pump control system

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4067664A (en) * 1974-12-31 1978-01-10 Robert Bosch Gmbh Control system for a pump
JPS525864A (en) * 1975-06-28 1977-01-17 Hehl Karl Controlling system for hydraulic pressure circuit of injection molder
JPS601170B2 (en) * 1975-06-28 1985-01-12 カール・ヘール Control device for fluid pressure circuit of injection molding machine
US4123202A (en) * 1975-11-04 1978-10-31 Plessey Handel Und Investments Ag Hydraulic pumping arrangements
US4118149A (en) * 1976-02-05 1978-10-03 Hytec Ab Output regulation in hydraulic and hydropneumatic systems
US4194364A (en) * 1977-05-21 1980-03-25 Robert Bosch Gmbh Arrangement for controlling the operation of a fluid-displacement machine
JPS5554701A (en) * 1978-09-28 1980-04-22 Eaton Corp Loaddresponsible controller for hydraulic system
JPH0255642B2 (en) * 1978-09-28 1990-11-28 Eaton Corp
US4194363A (en) * 1979-02-21 1980-03-25 General Signal Corporation Fluid horsepower control system
US4292805A (en) * 1979-09-24 1981-10-06 Rexnord Inc. Servo-valve convertible construction
JPH021522Y2 (en) * 1986-05-14 1990-01-16
JPH021521Y2 (en) * 1986-05-14 1990-01-16
JPS62801U (en) * 1986-05-14 1987-01-07
JPS61204002U (en) * 1986-05-14 1986-12-22
US4976106A (en) * 1988-02-18 1990-12-11 Linde Aktiengesellschaft Load-sensing variable displacement pump controller with adjustable pressure-compensated flow control valve in feedback path
US5203678A (en) * 1990-01-11 1993-04-20 Hitachi Construction Machinery Co., Ltd. Valve apparatus and hydraulic drive system
WO1994025770A3 (en) * 1993-04-28 1995-01-12 Roche Eng Corp Power sensing regenerator
WO1994025770A2 (en) * 1993-04-28 1994-11-10 Roche Engineering Corporation Power sensing regenerator
US5319932A (en) * 1993-04-28 1994-06-14 Roche Engineering Corporation Power sensing regenerator
AU677395B2 (en) * 1993-04-28 1997-04-24 Roche Engineering Corporation Power sensing regenerator
GB2279776A (en) * 1993-05-28 1995-01-11 Dana Corp A hydraulic load sensing system
GB2279776B (en) * 1993-05-28 1997-09-24 Dana Corp Hydraulic load sensing system
EP0869285A3 (en) * 1997-04-04 1999-09-22 Brueninghaus Hydromatik Gmbh Load sensing control with flushing circuit
US20050047930A1 (en) * 2002-03-06 2005-03-03 Johannes Schmid System for controlling a hydraulic variable-displacement pump
US20160003237A1 (en) * 2013-03-27 2016-01-07 Kayaba Industry Co., Ltd. Pump discharge flow-rate control device
CN103982475A (en) * 2014-05-30 2014-08-13 湖南五新重型装备有限公司 Hydraulic control system for concrete spraying vehicle boom frame
CN103982475B (en) * 2014-05-30 2016-03-02 湖南五新隧道智能装备股份有限公司 A kind of concrete ejection car jib hydraulic control system

Also Published As

Publication number Publication date
IT996264B (en) 1975-12-10
DE2350390C3 (en) 1979-08-30
CA983314A (en) 1976-02-10
SE383190B (en) 1976-03-01
JPS589276B2 (en) 1983-02-19
DE2350390A1 (en) 1974-07-04
JPS4989202A (en) 1974-08-26
GB1383490A (en) 1974-02-12
AU473650B2 (en) 1976-07-01
AU6028973A (en) 1975-03-13
FR2211054A5 (en) 1974-07-12
DE2350390B2 (en) 1979-01-11

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Owner name: SPERRY CORPORATION

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Effective date: 19790824

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Owner name: VICKERS, INCORPORATED TROY, MI A DE CORP

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST. EFFECTIVE NOVEMBER 2, 1983;ASSIGNOR:SPERRY CORPORATION A DE CORP.;REEL/FRAME:004337/0889

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Effective date: 19831102