DE68904740D1 - Lenkungsvorrichtung fuer ein fahrwerk. - Google Patents
Lenkungsvorrichtung fuer ein fahrwerk.Info
- Publication number
- DE68904740D1 DE68904740D1 DE8989403128T DE68904740T DE68904740D1 DE 68904740 D1 DE68904740 D1 DE 68904740D1 DE 8989403128 T DE8989403128 T DE 8989403128T DE 68904740 T DE68904740 T DE 68904740T DE 68904740 D1 DE68904740 D1 DE 68904740D1
- Authority
- DE
- Germany
- Prior art keywords
- chassis
- steering device
- steering
- 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 - Lifetime
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
- B64C25/505—Shimmy damping
-
- 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
- F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
- F15B15/02—Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member
- F15B15/06—Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member for mechanically converting rectilinear movement into non- rectilinear movement
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8815002A FR2639319A1 (fr) | 1988-11-18 | 1988-11-18 | Dispositif d'orientation d'un atterrisseur |
Publications (2)
Publication Number | Publication Date |
---|---|
DE68904740D1 true DE68904740D1 (de) | 1993-03-18 |
DE68904740T2 DE68904740T2 (de) | 1993-06-09 |
Family
ID=9371970
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8989403128T Expired - Lifetime DE68904740T2 (de) | 1988-11-18 | 1989-11-14 | Lenkungsvorrichtung fuer ein fahrwerk. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5002143A (de) |
EP (1) | EP0370865B1 (de) |
JP (1) | JPH07102837B2 (de) |
CA (1) | CA2003018C (de) |
DE (1) | DE68904740T2 (de) |
FR (1) | FR2639319A1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050241130A1 (en) * | 2004-04-28 | 2005-11-03 | Vinode Ramnauth | Apparatus for cleaning and processing two frameworks |
FR2887516B1 (fr) * | 2005-06-27 | 2008-10-03 | Messier Bugatti Sa | Architecture distribuee de systeme de gestion d'atterisseurs d'aeronef |
US20070054590A1 (en) * | 2005-08-24 | 2007-03-08 | Schmidt Christopher B | Photo-chromic toys |
US8899516B2 (en) | 2012-04-05 | 2014-12-02 | JHamilton Sundstrand Corporation | Coaxial contra-rotating motors for differential landing gear steering |
US8973866B2 (en) | 2012-04-10 | 2015-03-10 | Hamilton Sundstrand Corporation | Transverse flux machine utilized as part of a combined landing gear system |
FR3027015B1 (fr) * | 2014-10-10 | 2016-12-09 | Messier Bugatti Dowty | Atterrisseur d'aeronef. |
CN108216599B (zh) * | 2017-12-14 | 2021-04-20 | 中国航空工业集团公司成都飞机设计研究所 | 一种双联动大操纵角的前轮转弯机构 |
CN113998096B (zh) * | 2021-12-06 | 2023-02-10 | 西安航空制动科技有限公司 | 一种飞机电驱动系统的综合控制方法及系统 |
US11851167B2 (en) * | 2022-02-24 | 2023-12-26 | Goodrich Corporation | Integral steering motor and collar for landing gear |
EP4273041A1 (de) * | 2022-05-05 | 2023-11-08 | Goodrich Corporation | Integrierter lenkmotor und manschette für fahrwerk |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3124043A (en) * | 1964-03-10 | Fluid motor | ||
FR55352E (de) * | 1939-08-11 | 1952-07-09 | ||
US2958481A (en) * | 1956-07-02 | 1960-11-01 | Bendix Corp | Steering apparatus |
US3430896A (en) * | 1967-05-02 | 1969-03-04 | United Aircraft Corp | Shimmy damper |
US3904153A (en) * | 1974-02-25 | 1975-09-09 | Boeing Co | Steerable and retractable aircraft nose landing gear assembly |
US4313364A (en) * | 1979-06-04 | 1982-02-02 | Pneumo Corporation | Dual cylinder linear servo motor |
-
1988
- 1988-11-18 FR FR8815002A patent/FR2639319A1/fr active Granted
-
1989
- 1989-11-14 DE DE8989403128T patent/DE68904740T2/de not_active Expired - Lifetime
- 1989-11-14 EP EP89403128A patent/EP0370865B1/de not_active Expired - Lifetime
- 1989-11-15 CA CA002003018A patent/CA2003018C/fr not_active Expired - Lifetime
- 1989-11-15 US US07/436,775 patent/US5002143A/en not_active Expired - Lifetime
- 1989-11-17 JP JP1297749A patent/JPH07102837B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2639319A1 (fr) | 1990-05-25 |
FR2639319B1 (de) | 1994-12-23 |
EP0370865A1 (de) | 1990-05-30 |
JPH02182596A (ja) | 1990-07-17 |
JPH07102837B2 (ja) | 1995-11-08 |
US5002143A (en) | 1991-03-26 |
EP0370865B1 (de) | 1993-02-03 |
DE68904740T2 (de) | 1993-06-09 |
CA2003018C (fr) | 1994-02-22 |
CA2003018A1 (fr) | 1990-05-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |