GB820704A - Improvements in or relating to hydraulic motors - Google Patents

Improvements in or relating to hydraulic motors

Info

Publication number
GB820704A
GB820704A GB9412/58A GB941258A GB820704A GB 820704 A GB820704 A GB 820704A GB 9412/58 A GB9412/58 A GB 9412/58A GB 941258 A GB941258 A GB 941258A GB 820704 A GB820704 A GB 820704A
Authority
GB
United Kingdom
Prior art keywords
valve
line
piston
pressure
motor
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
Application number
GB9412/58A
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.)
Curtiss Wright Corp
Original Assignee
Curtiss Wright 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 Curtiss Wright Corp filed Critical Curtiss Wright Corp
Publication of GB820704A publication Critical patent/GB820704A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/08Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor
    • F15B11/15Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor with special provision for automatic return
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/70Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/71Multiple output members, e.g. multiple hydraulic motors or cylinders
    • F15B2211/7114Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators
    • F15B2211/7128Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators the chambers being connected in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/70Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/77Control of direction of movement of the output member
    • F15B2211/7725Control of direction of movement of the output member with automatic reciprocation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

820,704. Hydraulic control systems. CURTISS-WRIGHT CORPORATION. March 24, 1958 [March 25, 1957], No. 9412/58. Class 69(2). A control system for one or more reciprocating motors is such that the pressure of the hydraulic fluid supply can vary over a wide range without adversely affecting the operation of the motors. The motors are supplied through a throttle valve from a main hydraulic system, and a reversing valve which is actuated by the rise in motor-operating pressure at the end of each stroke, is restrained from actuation until the motor-operating pressure has risen to near the pressure then existing in the main system. Motors 17, 18 for actuating aircraft windscreen wipers are supplied with liquid from the aircraft hydraulic system via a line 2, an adjustable throttle valve, a line 7 and a reversing valve 16 alternately to motor lines 11, 14, the exhaust side being open via a valve chamber 20 to a line 15. Reversing valve 16 is actuated, through a quick-throw arrangement, by a piston 10 subject to the pressures in the motor lines 11, 14. Balancing pistons 24, 25 are provided in chambers on opposite sides of the piston 10 and are urged inwardly by the pressure in the aircraft system applied via a shut-off valve and a line 3, the inner faces of the pistons being subject to the pressure in the associated end of the cylinder of piston 10. Operation.-When a manually operable stem 33 of a master control and metering valve 1 is raised, the first operation is to admit liquid past valve seating surfaces 31<SP>1</SP> to the line 3 to move pistons 24, 25 inwards to centralize the valve actuator piston 10. Further opening movement of stem 33 permits a floating plug 31 to engage a shoulder 32<SP>1</SP> and further upward movement opens a bore in the plug to give throttled flow to the line 7. As shown, liquid is supplied to the line 11 to move the motor pistons to the right, the piston 10 being prevented by piston 25 from moving the quickthrow mechanism past dead centre. When the motor pistons are arrested the pressure in line 11 rises, and when it almost equals the then existing supply system pressure it is sufficient to move the piston 10 to the right to reverse valve 16 and initiate another stroke. By slowly closing the master control valve 1 the wipers can be parked at either end of the stroke. The quick-throw mechanism is described in U.S.A. Specification 2,451,449.
GB9412/58A 1957-03-25 1958-03-24 Improvements in or relating to hydraulic motors Expired GB820704A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US820704XA 1957-03-25 1957-03-25

Publications (1)

Publication Number Publication Date
GB820704A true GB820704A (en) 1959-09-23

Family

ID=22168873

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9412/58A Expired GB820704A (en) 1957-03-25 1958-03-24 Improvements in or relating to hydraulic motors

Country Status (1)

Country Link
GB (1) GB820704A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103410803A (en) * 2013-08-13 2013-11-27 常德中联重科液压有限公司 Pilot operated directional control valve, coordinated control hydraulic system and hydraulic control system of excavator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103410803A (en) * 2013-08-13 2013-11-27 常德中联重科液压有限公司 Pilot operated directional control valve, coordinated control hydraulic system and hydraulic control system of excavator
CN103410803B (en) * 2013-08-13 2015-11-25 常德中联重科液压有限公司 The hydraulic control system of pilot operated directional control valve, coordinated signals hydraulic system and excavator

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