ATE510767T1 - Flugzeugstruktur mit geänderter scharnierachse einer steuerungsvorrichtung - Google Patents

Flugzeugstruktur mit geänderter scharnierachse einer steuerungsvorrichtung

Info

Publication number
ATE510767T1
ATE510767T1 AT09706251T AT09706251T ATE510767T1 AT E510767 T1 ATE510767 T1 AT E510767T1 AT 09706251 T AT09706251 T AT 09706251T AT 09706251 T AT09706251 T AT 09706251T AT E510767 T1 ATE510767 T1 AT E510767T1
Authority
AT
Austria
Prior art keywords
control device
spar
actuator
aircraft structure
hinge axis
Prior art date
Application number
AT09706251T
Other languages
English (en)
Inventor
Robert James Heath
Original Assignee
Airbus Operations 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 Operations Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE510767T1 publication Critical patent/ATE510767T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Tires In General (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Transmitters (AREA)
AT09706251T 2008-01-31 2009-01-22 Flugzeugstruktur mit geänderter scharnierachse einer steuerungsvorrichtung ATE510767T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0801762.6A GB0801762D0 (en) 2008-01-31 2008-01-31 Aircraft structure with modified control device hinge line
PCT/GB2009/050055 WO2009095707A2 (en) 2008-01-31 2009-01-22 Aircraft structure with modified control device hinge line

Publications (1)

Publication Number Publication Date
ATE510767T1 true ATE510767T1 (de) 2011-06-15

Family

ID=39186634

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09706251T ATE510767T1 (de) 2008-01-31 2009-01-22 Flugzeugstruktur mit geänderter scharnierachse einer steuerungsvorrichtung

Country Status (5)

Country Link
US (1) US20100282898A1 (de)
EP (1) EP2238024B1 (de)
AT (1) ATE510767T1 (de)
GB (1) GB0801762D0 (de)
WO (1) WO2009095707A2 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2583134B (en) * 2019-04-18 2021-11-24 Fokker Aerostructures Bv Hinge structure

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2549760A (en) * 1949-04-14 1951-04-24 Adams George Kenneth Aerodynamic flap balance and auxiliary airfoil
US3020008A (en) * 1957-10-01 1962-02-06 Houdaille Industries Inc Control surface actuator damper hinge
US3594851A (en) * 1970-05-04 1971-07-27 Boeing Co Fail safe hinge and mounting
US5253828A (en) * 1992-07-17 1993-10-19 The Board Of Regents Of The University Of Oklahoma Concealable flap-actuated vortex generator
US5388788A (en) * 1993-12-16 1995-02-14 The Boeing Company Hinge fairings for control surfaces
US5941480A (en) * 1997-05-08 1999-08-24 Mcdonnell Douglas Hinge line skin system for an aircraft
US6257528B1 (en) * 1999-07-20 2001-07-10 The Boeing Company Vehicle control system and method employing control surface and geared tab
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

Also Published As

Publication number Publication date
EP2238024B1 (de) 2011-05-25
WO2009095707A3 (en) 2009-09-24
US20100282898A1 (en) 2010-11-11
WO2009095707A2 (en) 2009-08-06
GB0801762D0 (en) 2008-03-05
EP2238024A2 (de) 2010-10-13

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Legal Events

Date Code Title Description
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