JPS57501956A - - Google Patents
Info
- Publication number
- JPS57501956A JPS57501956A JP57500478A JP50047882A JPS57501956A JP S57501956 A JPS57501956 A JP S57501956A JP 57500478 A JP57500478 A JP 57500478A JP 50047882 A JP50047882 A JP 50047882A JP S57501956 A JPS57501956 A JP S57501956A
- Authority
- JP
- Japan
- 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.)
- Pending
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Retarders (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/218,772 US4392622A (en) | 1980-12-22 | 1980-12-22 | Combined beam support for landing gear |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS57501956A true JPS57501956A (ja) | 1982-11-04 |
Family
ID=22816448
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57500478A Pending JPS57501956A (ja) | 1980-12-22 | 1981-12-14 |
Country Status (5)
Country | Link |
---|---|
US (1) | US4392622A (ja) |
EP (1) | EP0067208B1 (ja) |
JP (1) | JPS57501956A (ja) |
DE (1) | DE3176308D1 (ja) |
WO (1) | WO1982002180A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2020175883A (ja) * | 2019-04-16 | 2020-10-29 | ザ・ボーイング・カンパニーThe Boeing Company | 航空機のメインランディングギアのドラッグブレースのバックアップ取付具アセンブリおよび関連方法 |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2320002A (en) * | 1996-12-04 | 1998-06-10 | British Aerospace | Aircraft landing gear arrangement |
US6131852A (en) * | 1998-02-18 | 2000-10-17 | British Aerospace Public Limited Company | Aircraft undercarriage locking system |
FR2795042B1 (fr) * | 1999-06-15 | 2001-10-12 | Aerospatiale Airbus | Avion comportant un train d'atterrissage a detachement controle en cas d'accident |
US6651928B1 (en) | 2002-09-05 | 2003-11-25 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
US6679452B1 (en) * | 2002-10-10 | 2004-01-20 | The Boeing Company | Aircraft landing gear support assemblies and associated methods of installation |
CA2579491C (en) | 2004-08-30 | 2014-02-18 | Messier-Dowty (Usa), Inc. | Dual brace-determinate landing gear |
FR2885596B1 (fr) * | 2005-05-12 | 2007-07-06 | Eurocopter France | Procede et systeme anti-crash, atterrisseur et aeronef |
US7798444B2 (en) * | 2007-09-24 | 2010-09-21 | The Boeing Company | Landing gear system and load distribution |
GB201114437D0 (en) | 2011-08-22 | 2011-10-05 | Airbus Operations Ltd | Landing gear attachment |
BR102013032347B1 (pt) * | 2013-12-16 | 2023-03-07 | Yaborã Indústria Aeronáutica S.A. | Fixação de trem de pouso de aeronave e aeronave |
EP2902316B1 (en) | 2014-02-04 | 2019-04-24 | Safran Landing Systems UK Limited | Aircraft assembly |
US9321524B2 (en) * | 2014-04-22 | 2016-04-26 | Goodrich Corporation | Bogie beam articulation mechanism |
US10442551B2 (en) * | 2015-11-16 | 2019-10-15 | The Boeing Company | Fuse pin model differential or exclusion feature |
US10160535B2 (en) * | 2015-11-16 | 2018-12-25 | The Boeing Company | Fuse pin model differential or exclusion feature |
FR3060535B1 (fr) * | 2016-12-15 | 2019-01-25 | Airbus Operations (S.A.S.) | Dispositif de protection de voilure d'aeronef contre les intemperies et procede de mise en place |
CN106628103B (zh) * | 2017-01-17 | 2023-07-18 | 深圳市哈威飞行科技有限公司 | 涵道飞行器的前起落架承力机构 |
US11130563B2 (en) * | 2018-11-07 | 2021-09-28 | The Boeing Company | Monolithic outboard gear beam support fitting |
IT201900019934A1 (it) * | 2019-10-29 | 2021-04-29 | Leonardo Spa | Maniglia a carico applicabile limitato per una porta di un aeromobile |
GB2601376A (en) * | 2020-11-30 | 2022-06-01 | Airbus Operations Ltd | Structural fuse |
CN112478140B (zh) * | 2020-12-02 | 2023-09-22 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种无人机起落架连接结构 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2123113A (en) * | 1935-02-04 | 1938-07-05 | Siam | Retractable landing gear for aeroplanes |
US2082598A (en) * | 1935-03-22 | 1937-06-01 | Saulnler Raymond | Airplane landing gear |
US2182333A (en) * | 1937-08-17 | 1939-12-05 | Cowey Leonard Eugene | Tail supporting wheel or its equivalent for aircraft |
DE732203C (de) * | 1940-02-02 | 1943-02-24 | Ernst Heinkel Flugzeugwerke G | Einschwenkbares Flugzeugfahrwerk |
US2318568A (en) * | 1940-03-15 | 1943-05-04 | Ohio Commw Eng Co | Hydraulic landing gear |
US2415615A (en) * | 1942-02-16 | 1947-02-11 | Edward E Wallace | Airplane |
US2474694A (en) * | 1944-07-25 | 1949-06-28 | Saulnier Raymond | Retractable landing gear for aircraft |
US2440068A (en) * | 1945-04-07 | 1948-04-20 | Bendix Aviat Corp | Supporting beam for aircraft landing gears |
US2476610A (en) * | 1946-07-17 | 1949-07-19 | Curtiss Wright Corp | Wheel brake for retracted landing gears |
US2562778A (en) * | 1946-11-27 | 1951-07-31 | Curtiss Wright Corp | Retractable landing gear |
US2559451A (en) * | 1947-09-12 | 1951-07-03 | Lockheed Aircraft Corp | Landing gear with drag strut dynamic damper |
US2630990A (en) * | 1951-03-01 | 1953-03-10 | Glenn L Martin Co | Retractable landing gear |
US2659555A (en) * | 1951-07-27 | 1953-11-17 | Boeing Co | Aircraft with quadricycle landing gear |
US2750134A (en) * | 1952-04-17 | 1956-06-12 | Lockheed Aircraft Corp | Multiple wheel main landing gear |
FR1467923A (fr) * | 1965-12-22 | 1967-02-03 | Hispano Suiza Lallemant Soc | Perfectionnements apportés aux trains d'atterrissage relevables |
FR2348851A1 (fr) * | 1976-04-22 | 1977-11-18 | Messier Hispano Sa | Train d'atterrissage comportant un dispositif de securite a charge de rupture predeterminee |
GB1521847A (en) * | 1976-04-30 | 1978-08-16 | Rolls Royce | Attachment for attaching jet propulsion engines to vehicle structure |
US4155522A (en) * | 1977-07-14 | 1979-05-22 | The Boeing Company | Overload release apparatus for aircraft landing gear or the like |
-
1980
- 1980-12-22 US US06/218,772 patent/US4392622A/en not_active Expired - Lifetime
-
1981
- 1981-12-14 DE DE8282900438T patent/DE3176308D1/de not_active Expired
- 1981-12-14 EP EP82900438A patent/EP0067208B1/en not_active Expired
- 1981-12-14 WO PCT/US1981/001673 patent/WO1982002180A1/en active IP Right Grant
- 1981-12-14 JP JP57500478A patent/JPS57501956A/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2020175883A (ja) * | 2019-04-16 | 2020-10-29 | ザ・ボーイング・カンパニーThe Boeing Company | 航空機のメインランディングギアのドラッグブレースのバックアップ取付具アセンブリおよび関連方法 |
Also Published As
Publication number | Publication date |
---|---|
EP0067208A4 (en) | 1984-12-11 |
EP0067208B1 (en) | 1987-07-15 |
EP0067208A1 (en) | 1982-12-22 |
WO1982002180A1 (en) | 1982-07-08 |
DE3176308D1 (en) | 1987-08-20 |
US4392622A (en) | 1983-07-12 |