DE2451887C3 - Flugzeugtragflügel - Google Patents

Flugzeugtragflügel

Info

Publication number
DE2451887C3
DE2451887C3 DE2451887A DE2451887A DE2451887C3 DE 2451887 C3 DE2451887 C3 DE 2451887C3 DE 2451887 A DE2451887 A DE 2451887A DE 2451887 A DE2451887 A DE 2451887A DE 2451887 C3 DE2451887 C3 DE 2451887C3
Authority
DE
Germany
Prior art keywords
flap
wing
nose
main wing
actuator
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
Application number
DE2451887A
Other languages
German (de)
English (en)
Other versions
DE2451887B2 (de
DE2451887A1 (de
Inventor
Serge Clichy Hauts-De- Seine Portier (Frankreich)
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE2451887A1 publication Critical patent/DE2451887A1/de
Publication of DE2451887B2 publication Critical patent/DE2451887B2/de
Application granted granted Critical
Publication of DE2451887C3 publication Critical patent/DE2451887C3/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/26—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by multiple flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering Devices For Bicycles And Motorcycles (AREA)
  • Blinds (AREA)
  • Check Valves (AREA)
  • Bridges Or Land Bridges (AREA)
  • Prostheses (AREA)
DE2451887A 1973-11-06 1974-10-31 Flugzeugtragflügel Expired DE2451887C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7339383A FR2249804B1 (enExample) 1973-11-06 1973-11-06

Publications (3)

Publication Number Publication Date
DE2451887A1 DE2451887A1 (de) 1975-06-19
DE2451887B2 DE2451887B2 (de) 1980-01-24
DE2451887C3 true DE2451887C3 (de) 1980-09-18

Family

ID=9127346

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2451887A Expired DE2451887C3 (de) 1973-11-06 1974-10-31 Flugzeugtragflügel

Country Status (4)

Country Link
US (1) US3949957A (enExample)
DE (1) DE2451887C3 (enExample)
FR (1) FR2249804B1 (enExample)
GB (1) GB1465125A (enExample)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4042191A (en) * 1976-05-03 1977-08-16 The Boeing Company Slot seal for leading edge flap
DE3105183C2 (de) * 1981-02-13 1986-09-25 Günther 2000 Hamburg Spranger Einrichtung zur Verminderung des Strömungswiderstandes von von Gasen wie Luft oder dergl. umströmten Flügeln
FR2695905B1 (fr) * 1992-09-24 1994-12-16 Aerospatiale Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
US6375126B1 (en) * 2000-11-16 2002-04-23 The Boeing Company Variable camber leading edge for an airfoil
FR2840877B1 (fr) * 2002-06-13 2004-08-06 Airbus France Dispositif d'articulation d'un volet sur une surface aerodynamique d'aeronef
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
EP1585665B1 (en) * 2003-01-23 2008-05-28 Bell Helicopter Textron Inc. Proprotor blade with leading edge slot
US7243881B2 (en) * 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
GB2417937B (en) * 2004-09-10 2009-08-12 Ultra Electronics Ltd An aircraft wing coupling arrangement
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7300021B2 (en) 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
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
US7475854B2 (en) * 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
DE102006053259A1 (de) * 2006-11-11 2008-05-21 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs und Verfahren zu seiner Betätigung
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8226048B2 (en) * 2008-12-09 2012-07-24 The Boeing Company Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
DE102009057340A1 (de) * 2009-12-07 2011-06-09 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug, Verfahren zum Bewegen einer Auftriebsklappe und Flugzeug mit einem Hochauftriebssystem
GB201009970D0 (en) * 2010-06-15 2010-07-21 Airbus Operations Ltd Telescopic strut
CN102501984B (zh) * 2011-10-19 2016-04-06 无锡市海航电液伺服系统股份有限公司 可计算襟翼丝杠加载的轴向力的襟翼加载装置
CN102501985B (zh) * 2011-10-19 2016-04-27 无锡市海航电液伺服系统股份有限公司 大飞机襟翼加载装置
US8622350B1 (en) * 2011-11-14 2014-01-07 The Boeing Company Compound leading edge device for aircraft
CN104691745B (zh) * 2014-07-04 2016-12-07 贵州贵航飞机设计研究所 薄翼型下使用一个作动筒完成双缝襟翼运动的方法及装置
MX2019003715A (es) * 2019-03-29 2020-09-30 Rosado Rodrigo Gallardo Ala rotativa de autorotacion inducida.
CN114340998B (zh) * 2019-10-09 2024-12-27 小鹰公司 用于不同飞行模式的混合功率系统
US11247773B2 (en) 2020-06-12 2022-02-15 Kitty Hawk Corporation Pylon mounted tilt rotor
US11655024B1 (en) 2022-05-25 2023-05-23 Kitty Hawk Corporation Battery systems with power optimized energy source and energy storage optimized source

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB517422A (en) * 1938-07-19 1940-01-30 Westland Aircraft Ltd Improvements in or relating to aircraft
US2776577A (en) * 1953-08-10 1957-01-08 Foote Bros Gear And Machine Co Screw actuating device
US3371888A (en) * 1965-07-12 1968-03-05 Alberto Alvarez Calderon Inverting flap system
US3556439A (en) * 1968-11-22 1971-01-19 Boeing Co Methods and high lift systems for making an aircraft wing more efficient for takeoffs and landings

Also Published As

Publication number Publication date
DE2451887B2 (de) 1980-01-24
FR2249804B1 (enExample) 1976-10-01
FR2249804A1 (enExample) 1975-05-30
DE2451887A1 (de) 1975-06-19
GB1465125A (en) 1977-02-23
US3949957A (en) 1976-04-13

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee