DE3760445D1 - Control system for a moving aerodynamic surface of an aircraft - Google Patents
Control system for a moving aerodynamic surface of an aircraftInfo
- Publication number
- DE3760445D1 DE3760445D1 DE8787401289T DE3760445T DE3760445D1 DE 3760445 D1 DE3760445 D1 DE 3760445D1 DE 8787401289 T DE8787401289 T DE 8787401289T DE 3760445 T DE3760445 T DE 3760445T DE 3760445 D1 DE3760445 D1 DE 3760445D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- control system
- aerodynamic surface
- moving aerodynamic
- moving
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Operated Clutches (AREA)
- Mechanical Control Devices (AREA)
- Catching Or Destruction (AREA)
- Details Of Aerials (AREA)
- Feedback Control In General (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8608652A FR2600035B1 (fr) | 1986-06-16 | 1986-06-16 | Systeme pour la commande d'une surface aerodynamique mobile d'un aeronef. |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3760445D1 true DE3760445D1 (en) | 1989-09-21 |
Family
ID=9336355
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8787401289T Expired DE3760445D1 (en) | 1986-06-16 | 1987-06-09 | Control system for a moving aerodynamic surface of an aircraft |
Country Status (7)
Country | Link |
---|---|
US (1) | US4765572A (de) |
EP (1) | EP0250293B1 (de) |
JP (1) | JPS632795A (de) |
CA (1) | CA1300114C (de) |
DE (1) | DE3760445D1 (de) |
ES (1) | ES2010710B3 (de) |
FR (1) | FR2600035B1 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4884748A (en) * | 1988-09-02 | 1989-12-05 | United Technologies Corporation | Fairing flap arrangement |
FR2737698B1 (fr) * | 1995-08-08 | 1997-10-24 | Aerospatiale | Systeme pour commander une gouverne articulee sur une structure d'un vehicule |
FR2748720B1 (fr) * | 1996-05-17 | 1998-07-24 | Aerospatiale | Systeme pour la commande d'un volet compensateur de gouverne d'aeronef |
US6257528B1 (en) * | 1999-07-20 | 2001-07-10 | The Boeing Company | Vehicle control system and method employing control surface and geared tab |
US8256710B2 (en) * | 2007-09-14 | 2012-09-04 | Spectrum Aeronautical, Llc | Live trim tabs |
US8876063B2 (en) * | 2007-12-10 | 2014-11-04 | The Boeing Company | Flight control using multiple actuators on primary control surfaces with tabs |
RU2444463C1 (ru) * | 2010-09-15 | 2012-03-10 | Открытое акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" им. И.И. Торопова" | Рулевой привод |
US9180961B2 (en) | 2013-01-28 | 2015-11-10 | The Boeing Company | Control surface for creating variable camber along a wing |
EP2805879B1 (de) * | 2013-05-22 | 2017-07-05 | Airbus Operations GmbH | Klappenanordnung für einen flügel eines flugzeugs und ein flugzeug mit einem flügel mit solch einer klappenanordnung |
CN104648657A (zh) * | 2013-11-22 | 2015-05-27 | 中国航空工业集团公司西安飞机设计研究所 | 一种可抑制振动的带调整片操纵面 |
CN104908956A (zh) * | 2015-05-21 | 2015-09-16 | 江西洪都航空工业集团有限责任公司 | 自动纠偏脚蹬弹簧机构 |
CN108082448B (zh) * | 2017-11-03 | 2022-10-28 | 中航通飞研究院有限公司 | 一种双腔液压助力器非线性补偿装置 |
CN113998095B (zh) * | 2021-11-08 | 2024-07-02 | 陕西千山航空电子有限责任公司 | 一种教练机后缘襟翼控制系统的控制方法 |
EP4331975A1 (de) * | 2022-09-01 | 2024-03-06 | Airbus Operations GmbH | Hinterkantensystem für einen flugzeugflügel, verfahren zum antrieb von steuerflächen eines flugzeugs, flugzeugflügel und flugzeug |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2395671A (en) * | 1940-09-26 | 1946-02-26 | Douglas Aircraft Co Inc | Control means for airfoils |
US2623717A (en) * | 1946-05-06 | 1952-12-30 | Sperry Corp | Control system for controlled airfoils of aircraft |
US2843344A (en) * | 1948-06-02 | 1958-07-15 | Gen Dynamics Corp | Aircraft trim tab control |
FR1142454A (fr) * | 1954-12-24 | 1957-09-18 | Bristol Aeroplane Co Ltd | Perfectionnements aux commandes de vol d'un avion |
US3378217A (en) * | 1966-09-02 | 1968-04-16 | Bendix Corp | Trim disconnect device for an aircraft control system |
US3790108A (en) * | 1972-11-13 | 1974-02-05 | Mc Donnell Douglas Corp | Redundant stabilizer control |
-
1986
- 1986-06-16 FR FR8608652A patent/FR2600035B1/fr not_active Expired
-
1987
- 1987-06-09 EP EP87401289A patent/EP0250293B1/de not_active Expired
- 1987-06-09 ES ES87401289T patent/ES2010710B3/es not_active Expired
- 1987-06-09 DE DE8787401289T patent/DE3760445D1/de not_active Expired
- 1987-06-12 US US07/061,145 patent/US4765572A/en not_active Expired - Lifetime
- 1987-06-16 JP JP62148162A patent/JPS632795A/ja active Pending
- 1987-06-16 CA CA000539756A patent/CA1300114C/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0250293A1 (de) | 1987-12-23 |
FR2600035B1 (fr) | 1988-10-21 |
FR2600035A1 (fr) | 1987-12-18 |
ES2010710B3 (es) | 1989-12-01 |
CA1300114C (fr) | 1992-05-05 |
JPS632795A (ja) | 1988-01-07 |
US4765572A (en) | 1988-08-23 |
EP0250293B1 (de) | 1989-08-16 |
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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 |