ES2126226T3 - Articulacion para aeronave que comprende una charnela y su dispositivo de control. - Google Patents

Articulacion para aeronave que comprende una charnela y su dispositivo de control.

Info

Publication number
ES2126226T3
ES2126226T3 ES95400849T ES95400849T ES2126226T3 ES 2126226 T3 ES2126226 T3 ES 2126226T3 ES 95400849 T ES95400849 T ES 95400849T ES 95400849 T ES95400849 T ES 95400849T ES 2126226 T3 ES2126226 T3 ES 2126226T3
Authority
ES
Spain
Prior art keywords
aircraft
hatch
articulation
control device
hinge
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 - Lifetime
Application number
ES95400849T
Other languages
English (en)
Inventor
Jean Louis Chavanne
Daniel Bonenfant
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
Application granted granted Critical
Publication of ES2126226T3 publication Critical patent/ES2126226T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64C9/02—Mounting or supporting thereof
    • 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)
  • Mechanical Control Devices (AREA)
  • Hinges (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Details Of Aerials (AREA)

Abstract

CON EL FIN DE REDUCIR EL ESFUERZO A APLICAR SOBRE EL ORGANO DE CONTROL DE UN TIMON (10) ARTICULADO SOBRE UNA ESTRUCTURA (12) POR BISAGRAS ALOJADAS EN MUESCAS (28) FORMADAS EN EL BORDE DE ATAQUE (16), SE ASOCIA A CADA BISAGRA UN DISPOSITIVO DE PROTECCION. ESTE DISPOSITIVO COMPRENDE UNA PLACA DE CIERRE (32) FIJADA SOBRE CADA CARA EXTERIOR DE LA ESTRUCTURA DE SOPORTE (12) ASI COMO UNA PIEZA DE CARENADO (42) FIJADA SOBRE EL TIMON (10), D MANERA A RODEAR LA BISAGRA. LA PLACA DE CIERRE (32) COMPRENDE RANURAS EN CASO DE BLOQUEO. LA INVENCION SE APLICA A CUALQUIER MAQUINA MOVIL EN UN FLUIDO Y QUE COMPRENDE TIMONES, Y EN PARTICULAR A LAS AERONAVES.
ES95400849T 1994-04-18 1995-04-14 Articulacion para aeronave que comprende una charnela y su dispositivo de control. Expired - Lifetime ES2126226T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9404594A FR2718707B1 (fr) 1994-04-18 1994-04-18 Dispositif de protection d'une charnière de gouverne, notamment pour aéronef.

Publications (1)

Publication Number Publication Date
ES2126226T3 true ES2126226T3 (es) 1999-03-16

Family

ID=9462209

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95400849T Expired - Lifetime ES2126226T3 (es) 1994-04-18 1995-04-14 Articulacion para aeronave que comprende una charnela y su dispositivo de control.

Country Status (6)

Country Link
US (1) US5622336A (es)
EP (1) EP0678447B1 (es)
CA (1) CA2146812C (es)
DE (1) DE69505874T2 (es)
ES (1) ES2126226T3 (es)
FR (1) FR2718707B1 (es)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2277716A1 (es) * 2004-12-31 2007-07-16 Airbus España, S.L. Tapa reforzada para ranuras en un contorno aerodinamico.
ES2277715A1 (es) * 2004-12-31 2007-07-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3451041B2 (ja) * 1999-09-17 2003-09-29 川崎重工業株式会社 フラップヒンジ機構およびその製造方法ならびにフラップヒンジ装置
AT409482B (de) * 2001-01-26 2002-08-26 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
JP4713778B2 (ja) * 2001-07-24 2011-06-29 富士重工業株式会社 翼構造およびその製造方法
DE10202440C1 (de) * 2002-01-22 2003-10-02 Eads Deutschland Gmbh Gelenk zur Verbindung einer Längsseite mit einer Oberseite von Bauteilen sowie flexibles Band zur Verwendung für ein derartiges Gelenk
DE10202439C1 (de) * 2002-01-22 2003-12-04 Eads Deutschland Gmbh Gelenk zur Verbindung von Bauteilen mit einander zugewandten Längsseiten sowie flexibles Band zur Verwendung für ein derartiges Gelenk
FR2840877B1 (fr) * 2002-06-13 2004-08-06 Airbus France Dispositif d'articulation d'un volet sur une surface aerodynamique d'aeronef
FI118122B (fi) * 2004-10-08 2007-07-13 Patria Aerostructures Oy Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale
US7229046B2 (en) * 2005-10-25 2007-06-12 Durant Cecil John Servo mounting system for direct drive of an aircraft control surface
GB0807395D0 (en) * 2008-04-23 2008-05-28 Airbus Uk Ltd Flight surface seal
ES2372035B1 (es) * 2009-12-18 2012-11-21 Airbus Operations S.L. Dispositivo de protección de zonas sensibles frente a impacto de objetos extraños.
ES2399262B1 (es) * 2010-12-31 2014-04-29 Airbus Operations, S.L. Herraje regulable para la instalación y ajuste de carenas en aeronaves.
JP5956803B2 (ja) * 2012-03-29 2016-07-27 一般社団法人日本航空宇宙工業会 飛行体の高揚力装置
US9505485B2 (en) * 2012-05-08 2016-11-29 Lockheed Martin Corporation Vortex generation
CN104386241B (zh) * 2014-11-04 2016-08-17 江西洪都航空工业集团有限责任公司 一种飞机舱盖有机玻璃透明件的保护罩
US10017239B2 (en) 2015-12-18 2018-07-10 Northrop Grumman Systems Corporation Dynamic conformal aerodynamic seal (CAS) for aircraft control surfaces
CN107226194B (zh) * 2016-03-23 2022-04-05 空中客车简化股份公司 密封装置以及相关联的飞行控制面机构和飞行器
US10532805B2 (en) * 2016-09-20 2020-01-14 Gulfstream Aerospace Corporation Airfoil for an aircraft having reduced noise generation
CN110225861B (zh) * 2016-11-11 2023-08-08 威罗门飞行公司 挤压的翼部保护系统和装置
US11427302B2 (en) * 2019-04-01 2022-08-30 Yaborã Indústria Aeronáutica S.A. Closure fairings for wing leading edge slat track openings
EP3904203A1 (en) * 2020-04-29 2021-11-03 Airbus Operations, S.L. Trailing edge for a composite lifting surface

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR524814A (fr) * 1917-04-05 1921-09-10 Gabriel Voisin Dispositif de couvre-joint pour les articulations d'ailerons d'aéroplanes
US2368702A (en) * 1943-04-08 1945-02-06 Raymond D Bourne Streamlined hinge line for aircraft
US2461745A (en) * 1944-12-28 1949-02-15 United Aircraft Corp Hinge structure for aircraft surfaces
US4213587A (en) * 1978-12-04 1980-07-22 The Boeing Company Hinge arrangement for control surfaces
US4470366A (en) * 1982-09-30 1984-09-11 The Boeing Company Continuous single flap hinge and seal device for flexible hydrofoils and the like
EP0397433B1 (en) * 1989-05-08 1997-04-16 Canon Kabushiki Kaisha Image processing apparatus
GB8910654D0 (en) * 1989-05-09 1989-06-21 British Aerospace Flexible closing device for a wing leading edge
GB8924982D0 (en) * 1989-11-06 1989-12-28 British Aerospace Fairing arrangement for aircraft
FR2670177B1 (fr) * 1990-12-05 1993-01-22 Snecma Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur.
US5253828A (en) * 1992-07-17 1993-10-19 The Board Of Regents Of The University Of Oklahoma Concealable flap-actuated vortex generator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2277716A1 (es) * 2004-12-31 2007-07-16 Airbus España, S.L. Tapa reforzada para ranuras en un contorno aerodinamico.
ES2277715A1 (es) * 2004-12-31 2007-07-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.
US7669800B2 (en) 2004-12-31 2010-03-02 Airbus Espana, S.L. Reinforced cover for gaps in an aerodynamic contour

Also Published As

Publication number Publication date
FR2718707B1 (fr) 1996-07-12
CA2146812A1 (fr) 1995-10-19
FR2718707A1 (fr) 1995-10-20
EP0678447B1 (fr) 1998-11-11
EP0678447A1 (fr) 1995-10-25
CA2146812C (fr) 2005-06-14
US5622336A (en) 1997-04-22
DE69505874D1 (de) 1998-12-17
DE69505874T2 (de) 1999-06-02

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