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FR2988072B1 - Aeronef - Google Patents

Aeronef

Info

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
Application number
FR1351763A
Other languages
English (en)
Other versions
FR2988072A1 (fr
Inventor
Bernhard Hauber
Tanja Muenz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of FR2988072A1 publication Critical patent/FR2988072A1/fr
Application granted granted Critical
Publication of FR2988072B1 publication Critical patent/FR2988072B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
FR1351763A 2012-03-16 2013-02-28 Aeronef Active FR2988072B1 (fr)

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 (7)

* Cited by examiner, † Cited by third party
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
CN110877714A (zh) * 2018-09-04 2020-03-13 庞巴迪公司 具有离合器架构的高升力致动系统
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

Family Cites Families (27)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
US20170283041A1 (en) 2017-10-05
DE102012005423A1 (de) 2013-09-19
FR2988072A1 (fr) 2013-09-20
US20140097292A1 (en) 2014-04-10

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