GB757705A - Fluid pressure operated systems - Google Patents

Fluid pressure operated systems

Info

Publication number
GB757705A
GB757705A GB927753A GB927753A GB757705A GB 757705 A GB757705 A GB 757705A GB 927753 A GB927753 A GB 927753A GB 927753 A GB927753 A GB 927753A GB 757705 A GB757705 A GB 757705A
Authority
GB
United Kingdom
Prior art keywords
valve
fluid
selector
pipe
jack
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
GB927753A
Inventor
Christopher Bernard Ve Neilson
Kenneth George Hancock
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.)
Electro Hydraulics Ltd
Original Assignee
Electro Hydraulics Ltd
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 Electro Hydraulics Ltd filed Critical Electro Hydraulics Ltd
Priority to GB927753A priority Critical patent/GB757705A/en
Publication of GB757705A publication Critical patent/GB757705A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • B64C25/44Actuating mechanisms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/22Operating mechanisms fluid
    • 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
    • F15B21/00Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)

Abstract

757,705. Aircraft controls. ELECTRO-HYDRAULICS, Ltd. June 18, 1954 [April 2, 1953], No. 9277/53. Class 4. [Also in GroupXXIX] In a fluid pressure-operated system for aircraft undercarriages, brakes, flaps, and steering mechanism, two pumps are provided, one operating the port services and the other the starboard services, and the system is so arranged that if one pump fails the other pump will supply fluid to both port and starboard services. The system comprises two pumps 2, 2a, driven by separate engines or electric motors and supplied with fluid from header tanks 1, la; it comprises also selectors 3, 3a, main undercarriage jacks 25, 25a and uplock jacks 26, 26a, nose undercarriage jack 27, nose undercarriage door jack 28 and steering jacks 30. One lever or electric switch operates both selectors 3, 3a. Main undercarriage jack 25 is supplied with fluid from pump 2 through pipes 36, selector 3, filter 33, pipe 37, and non-return valve 23. Fluid returns from the jack through shuttle valve 13, pipe 38, and another filter 33. A pipe 39 connects the selector 3 to the jack 26 via another shuttle valve 13. Pipes 40, 41 of smaller diameter than pipes 37, 38 connect the selector 3 to a second jack 25a and its unlock jack 26a which are operated by fluid from the pump 2 if the pump 2a fails. Jacks 25, 26 are similarly connected to the selector 3a by pipes 40a, 41a in case the pump 2 fails. The emergency operation of these jacks will only lower the undercarriage. Nose wheel jack 27 is connected by a pipe 410 to the pipe 37, a one-way restrictor valve 23b being provided. An emergency fluid supply from pump 2a is available through pipe 36a, selector 3a, pipes 38a, 40a, 146 and shuttle valve 53. Nose undercarriage door jack 28 is connected by a branch 431, a sequence valve 14 and a pipe 430. Pipes 42, 45, 46 and a shuttle valve 63 carry an emergency supply. For emergency operation of jacks 27 and 28, fluid from pump 2a is supplied via branch 146 from pipe 40a. Steering jacks 30 are supplied with fluid through another branch 44, a pressure maintaining valve 15, and a steering selector 4. Fluid from the jacks returns to the selector 3 via pipes 45, 42, 44. Flaps are actuated from the pump 2 through pipe 47, filter 330, flap selector 5, filter 33 and shuttle valve 21. The other end of the jack is connected through a pipe 49, release valve 22, and a filter 330 to the selector 5, and by pipes 50, 77 to the tank 1. The selector is actuated by solenoids. When a valve 520 in the selector is open the flaps are lowered and when a valve 530 is open they are raised. In an emergency, the flaps are actuated by an emergency flap selector 6 and the pump 2a whereby fluid is supplied through pipes 36a, 47a. The emergency supply will only lower the flaps. The pipes of the normal and emergency systems are of the same diameter. Brakes are supplied with fluid by branch pipe 58 via a non-return valve 17, pressurereducing valve 11 and brake control selector valve 10 which may be operated by foot motors 9. An accumulator 8 provides for emergency operation of the brakes. Fluid returns to the tank 1 via pipes 57, 55, 50, 77. Shuttle valves, construction of (Fig. 2). The normal pressure supply acts on a piston 64 and moves it to the right and thereby moves a valve 72 from its seat 73 and the fluid passes through a pipe 74 to the associated jack. When the emergency supply is in use, the fluid moves a valve 70 from its seat 71, movement of the valve 70 causing a valve 72 to close. The emergency supply passes through a pipe 67 and a restrictor valve 68 to the associated jack. Specifications 650,878 and 680,722 are referred to.
GB927753A 1953-04-02 1953-04-02 Fluid pressure operated systems Expired GB757705A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB927753A GB757705A (en) 1953-04-02 1953-04-02 Fluid pressure operated systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB927753A GB757705A (en) 1953-04-02 1953-04-02 Fluid pressure operated systems

Publications (1)

Publication Number Publication Date
GB757705A true GB757705A (en) 1956-09-26

Family

ID=9868866

Family Applications (1)

Application Number Title Priority Date Filing Date
GB927753A Expired GB757705A (en) 1953-04-02 1953-04-02 Fluid pressure operated systems

Country Status (1)

Country Link
GB (1) GB757705A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6465690B1 (en) 1999-03-26 2002-10-15 The Dow Chemical Company Process for the preparation of polyamino succinic acids and derivatives thereof
FR2907097A1 (en) * 2006-10-17 2008-04-18 Messier Bugatti Sa HYDRAULIC SYSTEM ARCHITECTURE OF AIRCRAFT AIRBORNE MANEUVER
FR2907096A1 (en) * 2006-10-17 2008-04-18 Messier Bugatti Sa HYDRAULIC SYSTEM ARCHITECTURE OF AIRCRAFT AIRBORNE MANEUVER
CN103818549A (en) * 2012-11-16 2014-05-28 哈尔滨飞机工业集团有限责任公司 Automatic hydraulic braking pressure supply device for unmanned aerial vehicle
CN103818550A (en) * 2012-11-16 2014-05-28 哈尔滨飞机工业集团有限责任公司 Airplane hydraulic brake and nose wheel steering mechanism
JP2014132189A (en) * 2012-12-04 2014-07-17 Sumitomo Precision Prod Co Ltd Leg ascending and descending electric hydraulic actuator system
WO2014201225A1 (en) * 2013-06-14 2014-12-18 Bombardier Inc. Apparatus and method for controlling landing gear
DE10330805B4 (en) * 2003-07-08 2015-07-30 Liebherr-Aerospace Lindenberg Gmbh Aircraft landing gear control
CN104890862A (en) * 2015-06-24 2015-09-09 中国航空工业集团公司西安飞机设计研究所 Undercarriage emergency putting control system
US9873503B2 (en) 2013-07-22 2018-01-23 Learjet Inc. Tailplane with positive camber
EP3418189A1 (en) * 2017-06-23 2018-12-26 Airbus Operations Limited Aircraft hydraulics

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6465690B1 (en) 1999-03-26 2002-10-15 The Dow Chemical Company Process for the preparation of polyamino succinic acids and derivatives thereof
DE10330805B4 (en) * 2003-07-08 2015-07-30 Liebherr-Aerospace Lindenberg Gmbh Aircraft landing gear control
US8136760B2 (en) 2006-10-17 2012-03-20 Messier-Bugatti-Dowty Architecture for a hydraulic system for operating aircraft landing gear
EP1914163A1 (en) * 2006-10-17 2008-04-23 Messier-Bugatti Architecture of a hydraulic system for manoeuvring aircraft landing gear
EP1914164A1 (en) * 2006-10-17 2008-04-23 Messier-Bugatti Architecture of a hydraulic system for manoeuvring the landing gear of an aircraft
US8028954B2 (en) 2006-10-17 2011-10-04 Messier-Bugatti Architecture for a hydraulic system for operating aircraft landing gear
FR2907096A1 (en) * 2006-10-17 2008-04-18 Messier Bugatti Sa HYDRAULIC SYSTEM ARCHITECTURE OF AIRCRAFT AIRBORNE MANEUVER
FR2907097A1 (en) * 2006-10-17 2008-04-18 Messier Bugatti Sa HYDRAULIC SYSTEM ARCHITECTURE OF AIRCRAFT AIRBORNE MANEUVER
CN103818550B (en) * 2012-11-16 2016-06-22 哈尔滨飞机工业集团有限责任公司 A kind of airplane hydraulic pressure brake and nose wheel steering mechanism
CN103818549A (en) * 2012-11-16 2014-05-28 哈尔滨飞机工业集团有限责任公司 Automatic hydraulic braking pressure supply device for unmanned aerial vehicle
CN103818550A (en) * 2012-11-16 2014-05-28 哈尔滨飞机工业集团有限责任公司 Airplane hydraulic brake and nose wheel steering mechanism
JP2014132189A (en) * 2012-12-04 2014-07-17 Sumitomo Precision Prod Co Ltd Leg ascending and descending electric hydraulic actuator system
EP2740944A3 (en) * 2012-12-04 2017-06-28 Sumitomo Precision Products Co., Ltd. Electro hydrostatic actuator system for retracting/extending landing gear
WO2014201225A1 (en) * 2013-06-14 2014-12-18 Bombardier Inc. Apparatus and method for controlling landing gear
CN105377696A (en) * 2013-06-14 2016-03-02 庞巴迪公司 Apparatus and method for controlling landing gear
CN105377696B (en) * 2013-06-14 2017-10-10 庞巴迪公司 Apparatus and method for controlling undercarriage
US10106248B2 (en) 2013-06-14 2018-10-23 Bombardier Inc. Apparatus and method for controlling landing gear
US9873503B2 (en) 2013-07-22 2018-01-23 Learjet Inc. Tailplane with positive camber
CN104890862B (en) * 2015-06-24 2017-01-18 中国航空工业集团公司西安飞机设计研究所 Undercarriage emergency putting control system
CN104890862A (en) * 2015-06-24 2015-09-09 中国航空工业集团公司西安飞机设计研究所 Undercarriage emergency putting control system
EP3418189A1 (en) * 2017-06-23 2018-12-26 Airbus Operations Limited Aircraft hydraulics
GB2563675A (en) * 2017-06-23 2018-12-26 Airbus Operations Ltd Aircraft hydraulics
US11260961B2 (en) 2017-06-23 2022-03-01 Airbus Operations Limited Aircraft hydraulics

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