FR2988072B1 - Aeronef - Google Patents
AeronefInfo
- Publication number
- FR2988072B1 FR2988072B1 FR1351763A FR1351763A FR2988072B1 FR 2988072 B1 FR2988072 B1 FR 2988072B1 FR 1351763 A FR1351763 A FR 1351763A FR 1351763 A FR1351763 A FR 1351763A FR 2988072 B1 FR2988072 B1 FR 2988072B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/36—Transmitting means without power amplification or where power amplification is irrelevant fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE201210005423 DE102012005423A1 (de) | 2012-03-16 | 2012-03-16 | Flugzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2988072A1 FR2988072A1 (fr) | 2013-09-20 |
FR2988072B1 true FR2988072B1 (fr) | 2016-12-02 |
Family
ID=49043768
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1351763A Active FR2988072B1 (fr) | 2012-03-16 | 2013-02-28 | Aeronef |
Country Status (3)
Country | Link |
---|---|
US (2) | US20140097292A1 (fr) |
DE (1) | DE102012005423A1 (fr) |
FR (1) | FR2988072B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0917693D0 (en) * | 2009-10-09 | 2009-11-25 | Goodrich Actuation Systems Ltd | Actuator arrangement |
US10538312B2 (en) | 2012-03-16 | 2020-01-21 | Liebherr-Aerospace Lindenberg Gmbh | Operating an aircraft with improved aileron and landing function |
EP3301017B1 (fr) * | 2016-09-30 | 2019-08-07 | Airbus Operations GmbH | Système d'entraînement et de guidage d'une surface de commande de bord de fuite |
US10730610B2 (en) * | 2017-04-20 | 2020-08-04 | Hamilton Sunstrand Corporation | Flight control system transmission |
EP3620372A1 (fr) * | 2018-09-04 | 2020-03-11 | Bombardier Inc. | Système d'actionnement hypersustentateur ayant une architecture d'embrayage |
GB201815106D0 (en) | 2018-09-17 | 2018-10-31 | Airbus Operations Ltd | Improved aircraft wing and flight control surface |
US11884394B2 (en) * | 2022-07-01 | 2024-01-30 | The Boeing Company | Wing assemblies with tandemly actuated flight control surfaces, aircraft, and related methods |
EP4470912A1 (fr) * | 2023-05-31 | 2024-12-04 | Airbus Operations GmbH | Système aérodynamique pour aéronef |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2402118A (en) * | 1941-12-22 | 1946-06-18 | Northrop Aircraft Inc | Roll control for airplanes |
US2583405A (en) * | 1944-09-06 | 1952-01-22 | Youngman Robert Talbot | Full span flap and aileron control |
US2580841A (en) * | 1946-10-02 | 1952-01-01 | Bendix Aviat Corp | Flap aileron for airplanes |
US2682381A (en) * | 1948-10-30 | 1954-06-29 | Northrop Aircraft Inc | Combined aileron and landing flap |
US2977068A (en) * | 1955-09-28 | 1961-03-28 | Power Jets Res & Dev Ltd | Jet propelled aircraft |
US2978204A (en) * | 1955-09-28 | 1961-04-04 | Power Jets Res & Dev Ltd | Aircraft flying control systems |
US2978207A (en) * | 1958-09-18 | 1961-04-04 | Power Jets Res & Dev Ltd | Aircraft with jet flaps |
US3070334A (en) * | 1960-06-16 | 1962-12-25 | Power Jets Res & Dev Ltd | Flying control system for aircraft |
US3155346A (en) * | 1961-10-13 | 1964-11-03 | Power Jets Res & Dev Ltd | Flying control system for aircraft |
US3469807A (en) * | 1967-10-06 | 1969-09-30 | Wren Aircraft Corp | Aircraft yaw correction means |
US3539133A (en) * | 1968-05-20 | 1970-11-10 | Robertson Aircraft Corp | Inherently stable tapered wing flaperon airplane |
US3659810A (en) * | 1968-05-20 | 1972-05-02 | James L Robertson | Inherently stable tapered wing flaperon airplane |
US3614028A (en) * | 1970-01-12 | 1971-10-19 | Mc Donnell Douglas Corp | Turbofan-powered stol aircraft |
US4049219A (en) * | 1975-02-03 | 1977-09-20 | The Boeing Company | Variable pivot trailing edge flap |
US4120470A (en) * | 1976-09-28 | 1978-10-17 | The Boeing Company | Efficient trailing edge system for an aircraft wing |
US4180222A (en) * | 1976-12-27 | 1979-12-25 | Lockheed Aircraft Corporation | Aileron segment control for a flaperon system |
US4146200A (en) * | 1977-09-14 | 1979-03-27 | Northrop Corporation | Auxiliary flaperon control for aircraft |
US4479620A (en) * | 1978-07-13 | 1984-10-30 | The Boeing Company | Wing load alleviation system using tabbed allerons |
US4485992A (en) * | 1981-09-10 | 1984-12-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Leading edge flap system for aircraft control augmentation |
US4796192A (en) * | 1985-11-04 | 1989-01-03 | The Boeing Company | Maneuver load alleviation system |
US5842666A (en) * | 1997-02-21 | 1998-12-01 | Northrop Grumman Coporation | Laminar supersonic transport aircraft |
DE19835191C1 (de) * | 1998-08-04 | 2000-04-20 | Daimler Chrysler Ag | Flugsteuerungseinrichtung zur Verbesserung der Längsstabilität eines geregelten Flugzeugs |
US7004428B2 (en) * | 2003-01-24 | 2006-02-28 | Aerion Corporation | Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings |
US7243881B2 (en) * | 2003-06-03 | 2007-07-17 | The Boeing Company | Multi-function trailing edge devices and associated methods |
US7367532B2 (en) * | 2005-01-31 | 2008-05-06 | John Libby | High lift longitudinal axis control system |
US7708231B2 (en) * | 2005-11-21 | 2010-05-04 | The Boeing Company | Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
US8024079B2 (en) * | 2008-05-20 | 2011-09-20 | The Boeing Company | Wing-body load alleviation for aircraft |
-
2012
- 2012-03-16 DE DE201210005423 patent/DE102012005423A1/de active Pending
-
2013
- 2013-02-28 FR FR1351763A patent/FR2988072B1/fr active Active
- 2013-03-14 US US13/803,985 patent/US20140097292A1/en not_active Abandoned
-
2017
- 2017-04-13 US US15/486,901 patent/US20170283041A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
DE102012005423A1 (de) | 2013-09-19 |
US20140097292A1 (en) | 2014-04-10 |
FR2988072A1 (fr) | 2013-09-20 |
US20170283041A1 (en) | 2017-10-05 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 4 |
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Effective date: 20160408 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |