GB757705A - Fluid pressure operated systems - Google Patents
Fluid pressure operated systemsInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/44—Actuating mechanisms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
-
- 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
- F15B21/00—Common 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.
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)
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 |
-
1953
- 1953-04-02 GB GB927753A patent/GB757705A/en not_active Expired
Cited By (23)
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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