ES2397802T3 - Fuselados de carenado de unión de aeronave con porciones fijas y móviles, y sistemas y métodos asociados - Google Patents

Fuselados de carenado de unión de aeronave con porciones fijas y móviles, y sistemas y métodos asociados Download PDF

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Publication number
ES2397802T3
ES2397802T3 ES08874230T ES08874230T ES2397802T3 ES 2397802 T3 ES2397802 T3 ES 2397802T3 ES 08874230 T ES08874230 T ES 08874230T ES 08874230 T ES08874230 T ES 08874230T ES 2397802 T3 ES2397802 T3 ES 2397802T3
Authority
ES
Spain
Prior art keywords
hyper
spoiler
wing
sustaining
fuselage
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
ES08874230T
Other languages
English (en)
Spanish (es)
Inventor
Douglas S. Lacy
Gregory S. Benn
James M. Wheaton
Gregory M. Santini
Seiya Sakurai
Lawrence D. Smith
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.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2397802T3 publication Critical patent/ES2397802T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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)
ES08874230T 2008-05-09 2008-05-09 Fuselados de carenado de unión de aeronave con porciones fijas y móviles, y sistemas y métodos asociados Active ES2397802T3 (es)

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 (1)

Publication Number Publication Date
ES2397802T3 true ES2397802T3 (es) 2013-03-11

Family

ID=40352012

Family Applications (1)

Application Number Title Priority Date Filing Date
ES08874230T Active ES2397802T3 (es) 2008-05-09 2008-05-09 Fuselados de carenado de unión de aeronave con porciones fijas y móviles, y sistemas y métodos asociados

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
JP5214025B2 (ja) 2013-06-19
WO2009136949A1 (en) 2009-11-12
EP2296964B1 (en) 2012-12-19
CN102015444A (zh) 2011-04-13
CN102015444B (zh) 2014-02-19

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