GB820704A - Improvements in or relating to hydraulic motors - Google Patents
Improvements in or relating to hydraulic motorsInfo
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/08—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor
- F15B11/15—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor with special provision for automatic return
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/71—Multiple output members, e.g. multiple hydraulic motors or cylinders
- F15B2211/7114—Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators
- F15B2211/7128—Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators the chambers being connected in parallel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/77—Control of direction of movement of the output member
- F15B2211/7725—Control 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.
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)
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 |
-
1958
- 1958-03-24 GB GB9412/58A patent/GB820704A/en not_active Expired
Cited By (2)
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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