GB1510554A - Aircraft undercarriage unit - Google Patents
Aircraft undercarriage unitInfo
- Publication number
- GB1510554A GB1510554A GB1402075A GB1402075A GB1510554A GB 1510554 A GB1510554 A GB 1510554A GB 1402075 A GB1402075 A GB 1402075A GB 1402075 A GB1402075 A GB 1402075A GB 1510554 A GB1510554 A GB 1510554A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shock absorber
- wheel
- leg
- oil
- filled
- 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
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/60—Oleo legs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
1510554 Aircraft undercarriages BRITISH AIRCRAFT CORP Ltd 31 March 1976 [4 April 1975] 14020/75 Heading B7G On landing, pivoting of a bogie beam 5 about its connection 4 with a shock absorber leg 1, due to contact of a rear wheel or wheel pair 7 with the ground, is arrested when a further shock absorber 8 is fully extended as shown, and the beam 5 then pivots about its connection 12 with the shock absorber 8, compressing the leg 1 until a forward wheel or wheel pair 6 touches down. The leg 1 has an oil-filled compartment 17 and a part oil, part air-filled compartment 16, the aperture 14 between them being controlled by a pin 15 of suitably varied crosssection. The shock absorber 8 is oil filled and has a valve 19 to allow freer contraction than expansion. A jack (not shown) initially tilts the beam 5 into the rearward-wheel-down position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1402075A GB1510554A (en) | 1976-03-31 | 1976-03-31 | Aircraft undercarriage unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1402075A GB1510554A (en) | 1976-03-31 | 1976-03-31 | Aircraft undercarriage unit |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1510554A true GB1510554A (en) | 1978-05-10 |
Family
ID=10033533
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1402075A Expired GB1510554A (en) | 1976-03-31 | 1976-03-31 | Aircraft undercarriage unit |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1510554A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4749152A (en) * | 1986-05-13 | 1988-06-07 | Messier-Hispano-Bugatti | Aircraft undercarriage of tilting-beam type and of reduced bulk |
EP0328395A2 (en) * | 1988-02-11 | 1989-08-16 | British Aerospace Public Limited Company | Aircraft undercarriage unit |
WO1999047416A1 (en) * | 1998-03-19 | 1999-09-23 | The B.F. Goodrich Company | Dual mode positioner for an aircraft landing gear axle beam |
WO2000066430A1 (en) * | 1999-04-29 | 2000-11-09 | The Boeing Company | Combined damper and truck positioner for landing gear |
US6182925B1 (en) | 1999-03-30 | 2001-02-06 | The Boeing Company | Semi-levered landing gear and auxiliary strut therefor |
US6575405B2 (en) | 1999-03-30 | 2003-06-10 | The Boeing Company | Control system and method for a semi-levered landing gear for an aircraft |
WO2009047367A2 (en) | 2007-10-09 | 2009-04-16 | Messier-Dowty Limited | Load detection in an aircraft landing gear |
CN103209891A (en) * | 2010-09-08 | 2013-07-17 | 梅西耶-道提有限公司 | Aircraft landing gear |
-
1976
- 1976-03-31 GB GB1402075A patent/GB1510554A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4749152A (en) * | 1986-05-13 | 1988-06-07 | Messier-Hispano-Bugatti | Aircraft undercarriage of tilting-beam type and of reduced bulk |
EP0328395A2 (en) * | 1988-02-11 | 1989-08-16 | British Aerospace Public Limited Company | Aircraft undercarriage unit |
EP0328395A3 (en) * | 1988-02-11 | 1989-10-11 | British Aerospace Public Limited Company | Aircraft undercarriage unit |
US4940197A (en) * | 1988-02-11 | 1990-07-10 | British Aerospace Public Limited Company | Aircraft undercarriage unit |
WO1999047416A1 (en) * | 1998-03-19 | 1999-09-23 | The B.F. Goodrich Company | Dual mode positioner for an aircraft landing gear axle beam |
US6308916B1 (en) | 1998-03-19 | 2001-10-30 | The B. F. Goodrich Company | Dual mode positioner for an aircraft landing gear axle beam |
US6182925B1 (en) | 1999-03-30 | 2001-02-06 | The Boeing Company | Semi-levered landing gear and auxiliary strut therefor |
US6345564B1 (en) | 1999-03-30 | 2002-02-12 | The Boeing Company | Semi-levered landing gear and auxiliary strut thereof |
US6575405B2 (en) | 1999-03-30 | 2003-06-10 | The Boeing Company | Control system and method for a semi-levered landing gear for an aircraft |
WO2000066430A1 (en) * | 1999-04-29 | 2000-11-09 | The Boeing Company | Combined damper and truck positioner for landing gear |
WO2009047367A2 (en) | 2007-10-09 | 2009-04-16 | Messier-Dowty Limited | Load detection in an aircraft landing gear |
CN103209891A (en) * | 2010-09-08 | 2013-07-17 | 梅西耶-道提有限公司 | Aircraft landing gear |
US9266606B2 (en) | 2010-09-08 | 2016-02-23 | Messier-Dowty Limited | Aircraft landing gear |
CN103209891B (en) * | 2010-09-08 | 2016-04-13 | 梅西耶-道提有限公司 | Undercarriage |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |