GB795399A - Improvements concerning hydraulic amplifier devices and systems - Google Patents

Improvements concerning hydraulic amplifier devices and systems

Info

Publication number
GB795399A
GB795399A GB36727/55A GB3672755A GB795399A GB 795399 A GB795399 A GB 795399A GB 36727/55 A GB36727/55 A GB 36727/55A GB 3672755 A GB3672755 A GB 3672755A GB 795399 A GB795399 A GB 795399A
Authority
GB
United Kingdom
Prior art keywords
valve
piston
pressure
fluid
valve piston
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
GB36727/55A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB795399A publication Critical patent/GB795399A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P29/00Arrangements for regulating or controlling electric motors, appropriate for both AC and DC motors
    • H02P29/0016Control of angular speed of one shaft without controlling the prime mover
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • 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
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

795,399. Fluid-pressure servomotor control systems. GENERAL ELECTRIC CO. Dec. 22, 1955 [Dec. 30, 1954; Dec. 30, 1954], No. 36727/55. Class 135. An hydraulic system comprises a valve piston 28, Fig. 1, movable in response to pressures in control chambers 13, 14 at each end thereof through which pressurized fluid is continuously supplied and passed through to a sump, independent pressure control means 11, 12 for each chamber, and pressure control means through which the pressure fluid is supplied to each chamber and the effect of which is varied by movement of the valve piston. As applied to a steering control surface 16 of a dirigible craft the valve piston 28 controls a servo piston 38 and the pressure controller 11 consists of a valve 49 actuated by a solenoid 18 under the control of a manually operated member 17 or an automatic pilot. The pressure control means 12 consists of a similar valve 44 linked to the control surface 16. Pressure fluid is supplied at 22 and passes through ports 23, 24 and annular restrictions 25, 26 to the chambers 13, 14 from which it escapes through passages 48, 45 and annular restrictions surrounding portions 50, 46 of the valves 49, 44 to exhaust ports 51, 47. Movement of the valve 49 causes a change in the resistance to fluid escaping through the exhaust port 51 thereby altering the pressure in the chamber 13 and causing movement of the valve piston 28 to admit pressure fluid to one side of the servo piston 38 and connect the other side to an exhaust port 34. The movement of the valve piston also causes a change in the resistances offered by the restrictions 25, 26 to arrest movement of the valve piston. The movement of the control surface 16 is transmitted to the valve 44 to alter the resistance presented to fluid escaping from the chamber 14 so that ultimately the valve piston 28 is recentred after the servo piston has moved an amount corresponding to the displacement of the member 17. In a modification, the servo piston is anchored to a fixed member and the servo cylinder 28 together with the housing for the valve piston 28 is connected to the control surface 16 so that " follow-up " is obtained without the connection from the control surface to the valve 44. The valve 44 is then connected through a solenoid to an attitude stabilization damper consisting of a rate gyro and an electrical amplifier so as to impose a further control on the valve piston 28. In this modification the valve 49 is actuated directly by a manually operated lever instead of through the solenoid 18. In a further modification, the servo piston actuates a valve controlling the motive fluid supply to an engine for controlling the speed thereof and the pressure in the chamber 14 is governed by a pump driven by the engine, the valve 49 being manually operated to select the engine speed. Alternatively the pressure in the chamber 13 may be governed by another pump so that the speed of the controlled engine may follow that of another machine. In a further modification, the servo piston 38 actuates a valve 69, Fig. 4, controlling the motive fluid supplied to an engine 64 and the latter drives an eccentric 66 which reciprocates a rod 67 connected through springs 60, 61 to masses 62, 63 connected to the valves 44b, 49b. The spring- mass assemblies 60, 62 and 61, 63 are arranged to have natural frequencies of vibration above and below the frequency at which the engine 64 is to be controlled. The position of the valve piston 28 may be indicated visually by a pointer. In a further modification, the two valves 44b, 49b, which are single rather than double landed, are oscillated electromagnetically by a winding energized by the output from an A.C. generator or a D.C. generator with a pronounced " ripple " and the valve piston 28 controls a variable speed hydraulic coupling in the drive between a power plant and the generator. When more than one generator is connected in parallel a further winding operative on the valve 44b only may be provided to equalize the loads on the generators.
GB36727/55A 1954-12-30 1955-12-22 Improvements concerning hydraulic amplifier devices and systems Expired GB795399A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US795399XA 1954-12-30 1954-12-30

Publications (1)

Publication Number Publication Date
GB795399A true GB795399A (en) 1958-05-21

Family

ID=22151187

Family Applications (1)

Application Number Title Priority Date Filing Date
GB36727/55A Expired GB795399A (en) 1954-12-30 1955-12-22 Improvements concerning hydraulic amplifier devices and systems

Country Status (1)

Country Link
GB (1) GB795399A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4094229A (en) * 1974-11-05 1978-06-13 Leonard Willie B Fluidic repeater

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4094229A (en) * 1974-11-05 1978-06-13 Leonard Willie B Fluidic repeater

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