DE68902023T2 - Bugradlenkvorrichtung eines flugzeuges. - Google Patents
Bugradlenkvorrichtung eines flugzeuges.Info
- Publication number
- DE68902023T2 DE68902023T2 DE8989402267T DE68902023T DE68902023T2 DE 68902023 T2 DE68902023 T2 DE 68902023T2 DE 8989402267 T DE8989402267 T DE 8989402267T DE 68902023 T DE68902023 T DE 68902023T DE 68902023 T2 DE68902023 T2 DE 68902023T2
- Authority
- DE
- Germany
- Prior art keywords
- airplane
- steering device
- wheel steering
- bow wheel
- bow
- 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 - Fee Related
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
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
- Retarders (AREA)
- Fluid-Damping Devices (AREA)
- Handcart (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8811100A FR2635498B1 (fr) | 1988-08-22 | 1988-08-22 | Dispositif de manoeuvre en orientation du train de roues de l'atterrisseur auxiliaire d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
DE68902023D1 DE68902023D1 (de) | 1992-08-13 |
DE68902023T2 true DE68902023T2 (de) | 1993-03-04 |
Family
ID=9369451
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8989402267T Expired - Fee Related DE68902023T2 (de) | 1988-08-22 | 1989-08-10 | Bugradlenkvorrichtung eines flugzeuges. |
Country Status (6)
Country | Link |
---|---|
US (1) | US4948069A (de) |
EP (1) | EP0356309B1 (de) |
JP (1) | JPH02164697A (de) |
CA (1) | CA1325625C (de) |
DE (1) | DE68902023T2 (de) |
FR (1) | FR2635498B1 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5242131A (en) * | 1992-04-08 | 1993-09-07 | The Boeing Company | Steerable landing gear |
FR2696989B1 (fr) * | 1992-10-16 | 1994-12-23 | Messier Bugatti | Dispositif de manÓoeuvre en orientation de roues équipant l'extrémité inférieure d'une jambe d'atterrisseur d'aéronef. |
US5613651A (en) * | 1994-12-08 | 1997-03-25 | The Boeing Company | Landing gear axle steering without walking beam |
US5575700A (en) * | 1995-05-08 | 1996-11-19 | Cohen; Allen J. | Landing gear for model airplanes |
US7621481B2 (en) * | 2004-09-03 | 2009-11-24 | Lockheed-Martin Corporation | Decoupled steering/planing air vehicle nose landing gear |
FR2884801B1 (fr) | 2005-04-22 | 2008-11-14 | Eurocopter France | Atterrisseur auxillaire de nez, structure porteuse et aeronef a voilure tournante |
US7513456B2 (en) * | 2005-05-13 | 2009-04-07 | The Boeing Company | Apparatus and method for reduced backlash steering tiller |
GB201209527D0 (en) * | 2012-05-29 | 2012-07-11 | Airbus Operations Ltd | Aircraft landing gear arrangement, a kit therefore, an aircraft comprising the same and a method of determining the angular position of an aircraft wheel |
GB2536500A (en) * | 2015-03-20 | 2016-09-21 | Airbus Operations Ltd | Steering Device for an aircraft |
RU2695967C1 (ru) * | 2018-11-02 | 2019-07-29 | Публичное акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Командный блок устройства управления передней опорой шасси самолета (варианты) |
RU2695942C1 (ru) * | 2018-11-02 | 2019-07-29 | Публичное акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Переключатель режимов управления передней опорой шасси самолета (варианты), узел переключателя и силовой каркас переключателя |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2650782A (en) * | 1951-09-18 | 1953-09-01 | Boeing Co | Landing unit for aircraft |
US2930547A (en) * | 1955-06-17 | 1960-03-29 | Cleveland Pneumatic Ind Inc | Landing gear steering mechanism |
FR1159446A (fr) * | 1956-03-21 | 1958-06-27 | Cleveland Pneumatic Tool Co | Mécanisme de braquage perfectionné pour aéronefs |
US2838944A (en) * | 1957-05-28 | 1958-06-17 | Menasco Mfg Company | Linkage mechanism |
GB901836A (en) * | 1959-09-17 | 1962-07-25 | Dowty Rotol Ltd | Improvements in or relating to mechanisms for actuating swivelling actions |
JPS5711840U (de) * | 1980-06-25 | 1982-01-21 |
-
1988
- 1988-08-22 FR FR8811100A patent/FR2635498B1/fr not_active Expired - Lifetime
-
1989
- 1989-08-10 DE DE8989402267T patent/DE68902023T2/de not_active Expired - Fee Related
- 1989-08-10 EP EP89402267A patent/EP0356309B1/de not_active Expired - Lifetime
- 1989-08-11 JP JP1207027A patent/JPH02164697A/ja active Pending
- 1989-08-11 CA CA000608127A patent/CA1325625C/fr not_active Expired - Fee Related
- 1989-08-11 US US07/392,583 patent/US4948069A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2635498A1 (fr) | 1990-02-23 |
JPH02164697A (ja) | 1990-06-25 |
EP0356309B1 (de) | 1992-07-08 |
EP0356309A1 (de) | 1990-02-28 |
CA1325625C (fr) | 1993-12-28 |
DE68902023D1 (de) | 1992-08-13 |
US4948069A (en) | 1990-08-14 |
FR2635498B1 (fr) | 1990-11-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |