JP5214025B2 - 固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法 - Google Patents

固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法 Download PDF

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Publication number
JP5214025B2
JP5214025B2 JP2011508472A JP2011508472A JP5214025B2 JP 5214025 B2 JP5214025 B2 JP 5214025B2 JP 2011508472 A JP2011508472 A JP 2011508472A JP 2011508472 A JP2011508472 A JP 2011508472A JP 5214025 B2 JP5214025 B2 JP 5214025B2
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JP
Japan
Prior art keywords
flap
fillet
wing
fuselage
spoiler
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
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JP2011508472A
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English (en)
Japanese (ja)
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JP2011519782A (ja
JP2011519782A5 (enExample
Inventor
ダグラス エス． レーシー，
グレゴリー エス． ベン，
ジェームス エム． ホイートン，
グレゴリー エム． サンティニ，
セイヤ サクライ，
ローレンス ディ． スミス，
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.)
Boeing Co
Original Assignee
Boeing Co
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.)
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Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of JP2011519782A publication Critical patent/JP2011519782A/ja
Publication of JP2011519782A5 publication Critical patent/JP2011519782A5/ja
Application granted granted Critical
Publication of JP5214025B2 publication Critical patent/JP5214025B2/ja
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/58—Wings provided with fences or spoilers
    • 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
    • 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
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
JP2011508472A 2008-05-09 2008-05-09 固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法 Active JP5214025B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2008/063326 WO2009136949A1 (en) 2008-05-09 2008-05-09 Aircraft fillet fairings with fixed and moveable portions, and associated systems and methods

Publications (3)

Publication Number Publication Date
JP2011519782A JP2011519782A (ja) 2011-07-14
JP2011519782A5 JP2011519782A5 (enExample) 2011-08-25
JP5214025B2 true JP5214025B2 (ja) 2013-06-19

Family

ID=40352012

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011508472A Active JP5214025B2 (ja) 2008-05-09 2008-05-09 固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法

Country Status (6)

Country Link
EP (1) EP2296964B1 (enExample)
JP (1) JP5214025B2 (enExample)
CN (1) CN102015444B (enExample)
CA (1) CA2716169C (enExample)
ES (1) ES2397802T3 (enExample)
WO (1) WO2009136949A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011013828A1 (de) 2011-03-14 2012-09-20 Airbus Operations Gmbh Verkleidungsübergang und Fahrzeug mit einem bewegbaren und einem feststehenden Körper mit einem Verkleidungsübergang
CN103466077B (zh) * 2013-08-23 2016-09-14 中国航空工业集团公司西安飞机设计研究所 一种滚轮触发装置
FR3018767B1 (fr) 2014-03-21 2018-01-12 Airbus Operations Ensemble de support pour un systeme de volet d'aile d'un avion.
US10919614B2 (en) 2017-09-06 2021-02-16 Airbus Operations Gmbh Airfoil with a main wing and a high-lift body
CA3084642A1 (en) * 2019-06-24 2020-12-24 Bombardier Inc. Wing to fuse junction shaping, and associated systems and methods
US11932377B2 (en) 2021-06-04 2024-03-19 The Boeing Company Actuation mechanism for controlling aircraft surfaces

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526929A (en) * 1948-05-29 1950-10-24 Curtiss Wright Corp Airplane flap extension
GB1379814A (en) * 1972-03-14 1975-01-08 Secr Defence Aircraft wing flaps
DE3149629C1 (de) * 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe
US4576347A (en) * 1984-10-30 1986-03-18 The Boeing Company Flap torque tube slot seal
DE9113090U1 (de) * 1991-10-21 1992-01-16 Rochelt, Günter, Prof., 2000 Hamburg Flügel oder flügelartiges Bauteil
CN1061005C (zh) * 1995-03-15 2001-01-24 乐正伟 一种飞机翼梢引射器
DE29703039U1 (de) * 1997-02-20 1997-07-10 Droxner, Thomas, 80939 München Spaltfreie Klappenabdichtung
GB2324351A (en) * 1997-04-18 1998-10-21 British Aerospace Reducing drag in aircraft wing assembly
FR2892999B1 (fr) * 2005-11-08 2008-02-01 Airbus France Sas Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales
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
ES2301360B1 (es) * 2006-05-16 2009-05-01 Airbus España, S.L. Sistema de sellado del hueco existente entre el fuselaje y el timon de altura del estabilizador horizontal orientable de un avion, extendido con una carena aerodinamica de sellado de la abertura existente entre el fuselaje y el estabilizador horizontal orientable.

Also Published As

Publication number Publication date
EP2296964A1 (en) 2011-03-23
JP2011519782A (ja) 2011-07-14
CA2716169A1 (en) 2009-11-12
CA2716169C (en) 2013-12-17
WO2009136949A1 (en) 2009-11-12
EP2296964B1 (en) 2012-12-19
CN102015444A (zh) 2011-04-13
ES2397802T3 (es) 2013-03-11
CN102015444B (zh) 2014-02-19

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