ES2030173T3 - Flaps de borde de salida para alas de aviones. - Google Patents

Flaps de borde de salida para alas de aviones.

Info

Publication number
ES2030173T3
ES2030173T3 ES198888307388T ES88307388T ES2030173T3 ES 2030173 T3 ES2030173 T3 ES 2030173T3 ES 198888307388 T ES198888307388 T ES 198888307388T ES 88307388 T ES88307388 T ES 88307388T ES 2030173 T3 ES2030173 T3 ES 2030173T3
Authority
ES
Spain
Prior art keywords
wing
actuator
levers
trigger
car
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
ES198888307388T
Other languages
English (en)
Inventor
George Harry Williams
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Application granted granted Critical
Publication of ES2030173T3 publication Critical patent/ES2030173T3/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
    • B64C9/14—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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • 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)
  • Transmission Devices (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

ALERON DE BORDE POSTERIOR PARA ALA DE AERONAVE QUE INCLUYE EN SU EXTREMO POSTERIOR UNAS SUPERFICIES SUPERIOR E INFERIOR QUE TERMINAN EN UN BORDE POSTERIOR. EL SISTEMA TIENE UN ALERON (15) EN POSICION DE ESTIBA DURANTE EL VUELO NORMAL. UNA VIGUETA (18) VA SITUADA EN LA SUPERFICIE INFERIOR (12) DEL ALA, EXTENDIENDOSE HACIA ATRAS DE LA MISMA Y POR DEBAJO DEL ALERON (15). UN CARRO (23) VA ACOPLADO EN LA RODADURA CON GUIAS LONGITUDINALES (53) DE LA VIGUETA (18). PARA ACCIONAR EL ALERON (15) EXISTE EN EL EXTREMO POSTERIOR, O CERCA DE EL, DE LA VIGUETA (18) UNA ABRAZADERA (21) DE MONTAJE DEL ACTUADOR, UN ACTUADOR GIRATORIO (52) Y BRAZOS DE PALANCA (26,28) ASOCIADOS CON EL MISMO EN TORNO A UN EJE COMUN TRANSVERSAL DE ROTACION. LAS PALANCAS (26,28) SE EXTIENDEN HACIA ARRIBA Y TERMINAN ADYACENTES A LA SUPERFICIE INFERIOR DEL ALERON (15), EXISTIENDO, EN CONEXION PIVOTANTE (22), UNOS ENLACES DE ACTUADOR (25,26) QUE SE EXTIENDEN HACIA ADELANTE Y CONECTAN PIVOTALMENTE LAS PALANCAS (27,28) Y EL CARRO(23). EL ALERON (15) VA SUJETO MEDIANTE UN PRIMER ENLACE (33) QUE CONECTA EL CARRO (23) A UNA PARTE ANTERIOR DEL ALERON (15) Y UN SEGUNDO ENLACE (36) QUE CONECTA LOS ENLACES DE ACTUADOR (25,26) A UNA POSICION MAS RETRASADA DEL ALERON (15). EL POSICIONAMIENTO DE UN ACTUADOR (52) EN EL EXTREMO POSTERIOR DE LA VIGUETA (18) Y EN ACOPLAMIENTO DIRECTO CON UNA PALANCA ACTUADORA (27,28), ACOPLADA ESTRECHAMENTE CON EL ALERON (15), ES EFICAZ Y REDUCE LOS REQUERIMIENTOS ENERGETICOS.
ES198888307388T 1987-08-11 1988-08-10 Flaps de borde de salida para alas de aviones. Expired - Lifetime ES2030173T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB878718977A GB8718977D0 (en) 1987-08-11 1987-08-11 Trailing edge flaps

Publications (1)

Publication Number Publication Date
ES2030173T3 true ES2030173T3 (es) 1992-10-16

Family

ID=10622125

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198888307388T Expired - Lifetime ES2030173T3 (es) 1987-08-11 1988-08-10 Flaps de borde de salida para alas de aviones.

Country Status (7)

Country Link
US (1) US4840331A (es)
EP (1) EP0303458B1 (es)
JP (1) JPS6467495A (es)
BR (1) BR8804054A (es)
DE (1) DE3868774D1 (es)
ES (1) ES2030173T3 (es)
GB (1) GB8718977D0 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8821220D0 (en) * 1988-09-09 1988-12-14 British Aerospace Fuselage mounted flap drive for wing trailing edge flaps
DE4107556C1 (es) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US6299108B1 (en) * 1997-12-12 2001-10-09 Jeffrey V. Lindstrom Method and apparatus for detecting skew and asymmetry of an airplane flap
AT410656B (de) * 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten
DE102004006940B4 (de) * 2004-02-12 2009-02-26 Airbus Deutschland Gmbh Landeklappenführung für Luftfahrzeuge
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
CN104554709B (zh) * 2013-10-21 2016-08-24 哈尔滨飞机工业集团有限责任公司 一种襟翼运动限动机构
DE102014106930A1 (de) 2014-05-16 2015-11-19 Airbus Operations Gmbh Lasttragendes Verkleidungselement für eine Klappenverstellmechanik und Flugzeug mit einem solchen Verkleidungselement
CA3046256A1 (en) * 2018-06-18 2019-12-18 Bombardier Inc. Aircraft wing with deployable flap
EP4286272A1 (en) * 2022-05-31 2023-12-06 Airbus Operations GmbH Actuator arrangement and wing assembly for an aircraft
US20240002037A1 (en) * 2022-06-29 2024-01-04 The Boeing Company Failsafe determinate flap support underwing attachment

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1496518A (en) * 1975-10-08 1977-12-30 British Aircraft Corp Ltd Aircraft wings
US4381093A (en) * 1980-10-07 1983-04-26 The Boeing Company Flap assembly for aircraft wing
US4542869A (en) * 1983-06-23 1985-09-24 Mcdonnell Douglas Corporation Flap mechanism
DE3522448A1 (de) * 1985-06-22 1987-01-02 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer eine an einem flugzeugtragfluegel angeordnete klappe

Also Published As

Publication number Publication date
BR8804054A (pt) 1989-03-07
EP0303458A3 (en) 1989-11-29
EP0303458B1 (en) 1992-03-04
DE3868774D1 (de) 1992-04-09
JPS6467495A (en) 1989-03-14
US4840331A (en) 1989-06-20
GB8718977D0 (en) 1987-09-16
EP0303458A2 (en) 1989-02-15

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