ATE236044T1 - Stromlinienverkleidungen für flugzeuge - Google Patents

Stromlinienverkleidungen für flugzeuge

Info

Publication number
ATE236044T1
ATE236044T1 AT00954775T AT00954775T ATE236044T1 AT E236044 T1 ATE236044 T1 AT E236044T1 AT 00954775 T AT00954775 T AT 00954775T AT 00954775 T AT00954775 T AT 00954775T AT E236044 T1 ATE236044 T1 AT E236044T1
Authority
AT
Austria
Prior art keywords
aileron
fairing
overlap
wing
movement
Prior art date
Application number
AT00954775T
Other languages
English (en)
Inventor
Kim Sharp
Original Assignee
Airbus Uk Ltd
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 Uk Ltd filed Critical Airbus Uk Ltd
Application granted granted Critical
Publication of ATE236044T1 publication Critical patent/ATE236044T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Insulated Conductors (AREA)
  • Toys (AREA)
  • Laminated Bodies (AREA)
  • Radio Relay Systems (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Fluid-Pressure Circuits (AREA)
AT00954775T 1999-08-27 2000-08-25 Stromlinienverkleidungen für flugzeuge ATE236044T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9920318.4A GB9920318D0 (en) 1999-08-27 1999-08-27 A fairing arrangement for an aircraft
PCT/GB2000/003270 WO2001015972A1 (en) 1999-08-27 2000-08-25 A fairing arrangement for an aircraft

Publications (1)

Publication Number Publication Date
ATE236044T1 true ATE236044T1 (de) 2003-04-15

Family

ID=10859922

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00954775T ATE236044T1 (de) 1999-08-27 2000-08-25 Stromlinienverkleidungen für flugzeuge

Country Status (10)

Country Link
US (1) US6450457B1 (de)
EP (1) EP1206382B1 (de)
JP (1) JP3655586B2 (de)
AT (1) ATE236044T1 (de)
AU (1) AU6713000A (de)
CA (1) CA2382773C (de)
DE (1) DE60001964T2 (de)
ES (1) ES2192540T3 (de)
GB (1) GB9920318D0 (de)
WO (1) WO2001015972A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems 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
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
DE102005062190B3 (de) * 2005-12-23 2007-06-14 Airbus Deutschland Gmbh Verfahren zum Herstellen einer lösbaren Dichtung mit einer Dichtmasse sowie Verwendung von Klebestreifen zur Durchführung des Verfahrens
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
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
CN103596840A (zh) * 2011-06-16 2014-02-19 萨博公司 用于覆盖在飞行器的两个结构部之间的缝隙的双曲覆盖件
US9505485B2 (en) * 2012-05-08 2016-11-29 Lockheed Martin Corporation Vortex generation
GB201522486D0 (en) * 2015-12-21 2016-02-03 Airbus Operations Ltd Seal assembly
EP3318783A1 (de) * 2016-11-02 2018-05-09 Airbus Operations GmbH Verkleidung für ein flugzeug
GB2580930A (en) * 2019-01-30 2020-08-05 Airbus Operations Ltd Fairing for folding wing tip

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4705236A (en) * 1981-09-29 1987-11-10 The Boeing Company Aileron system for aircraft and method of operating the same
US4962902A (en) 1989-03-20 1990-10-16 The Boeing Company Aircraft control surface linkage
GB8919057D0 (en) * 1989-08-22 1989-10-04 British Aerospace Fairing arrangements for aircraft
GB8921749D0 (en) * 1989-09-27 1989-11-08 British Aerospace Fairing arrangements for aircraft
GB8924982D0 (en) 1989-11-06 1989-12-28 British Aerospace Fairing arrangement for aircraft
US5098043A (en) * 1990-02-27 1992-03-24 Grumman Aerospace Corporation Integrated power hinge actuator
US5388788A (en) 1993-12-16 1995-02-14 The Boeing Company Hinge fairings for control surfaces
US5915653A (en) * 1996-01-02 1999-06-29 The Boeing Company Spherical mating fairings for hingeline applications
GB2323576B (en) 1997-03-26 2001-08-22 British Aerospace Fairing arrangements for aircraft

Also Published As

Publication number Publication date
ES2192540T3 (es) 2003-10-16
GB9920318D0 (en) 1999-11-03
US6450457B1 (en) 2002-09-17
AU6713000A (en) 2001-03-26
CA2382773C (en) 2008-11-18
CA2382773A1 (en) 2001-03-08
EP1206382B1 (de) 2003-04-02
DE60001964T2 (de) 2003-11-06
JP3655586B2 (ja) 2005-06-02
EP1206382A1 (de) 2002-05-22
JP2003508287A (ja) 2003-03-04
DE60001964D1 (de) 2003-05-08
WO2001015972A1 (en) 2001-03-08

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties