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ES2192540T3 - Una disposicion de carenado para un avion. - Google Patents

Una disposicion de carenado para un avion.

Info

Publication number
ES2192540T3
ES2192540T3 ES00954775T ES00954775T ES2192540T3 ES 2192540 T3 ES2192540 T3 ES 2192540T3 ES 00954775 T ES00954775 T ES 00954775T ES 00954775 T ES00954775 T ES 00954775T ES 2192540 T3 ES2192540 T3 ES 2192540T3
Authority
ES
Spain
Prior art keywords
aileron
fairing
overlap
wing
movement
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
ES00954775T
Other languages
English (en)
Inventor
Kim Sharp
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 Operations Ltd
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 ES2192540T3 publication Critical patent/ES2192540T3/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
    • B64C7/00—Structures or fairings not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Insulated Conductors (AREA)
  • Laminated Bodies (AREA)
  • Radio Relay Systems (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

Una disposición de carenado (28) para un ala de avión (10) que comprende una primera porción de carenado (32) en el ala (10) y una segunda porción de carenado (34) en una superficie de control (12) montada en el ala (10), para desplazamiento angular en relación con el ala (10), sobresaliendo la disposición de carenado (28) hacia fuera de un perfil aerodinámico del ala (S) y de la superficie de control (12), siendo el desplazamiento angular de la superficie de control (12), al menos a lo largo de un rango de movimientos de funcionamiento normal, entre los límites positivo y negativo a cada lado de una posición de vuelo recto y nivelado, caracterizada porque se dispone un solape con conicidad entre la primera y la segunda porciones de carenado (32, 34), básicamente para formar un sello aerodinámico (45) al menos dentro de dicho rango de funcionamiento normal.
ES00954775T 1999-08-27 2000-08-25 Una disposicion de carenado para un avion. Expired - Lifetime ES2192540T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9920318.4A GB9920318D0 (en) 1999-08-27 1999-08-27 A fairing arrangement for an aircraft

Publications (1)

Publication Number Publication Date
ES2192540T3 true ES2192540T3 (es) 2003-10-16

Family

ID=10859922

Family Applications (1)

Application Number Title Priority Date Filing Date
ES00954775T Expired - Lifetime ES2192540T3 (es) 1999-08-27 2000-08-25 Una disposicion de carenado para un avion.

Country Status (10)

Country Link
US (1) US6450457B1 (es)
EP (1) EP1206382B1 (es)
JP (1) JP3655586B2 (es)
AT (1) ATE236044T1 (es)
AU (1) AU6713000A (es)
CA (1) CA2382773C (es)
DE (1) DE60001964T2 (es)
ES (1) ES2192540T3 (es)
GB (1) GB9920318D0 (es)
WO (1) WO2001015972A1 (es)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7258308B2 (en) 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
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
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
DE102005062190B3 (de) * 2005-12-23 2007-06-14 Airbus Deutschland Gmbh Verfahren zum Herstellen einer lösbaren Dichtung mit einer Dichtmasse sowie Verwendung von Klebestreifen zur Durchführung des Verfahrens
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
ES2602122T3 (es) * 2011-06-16 2017-02-17 Saab Ab Cubierta de doble curvatura para cubrir un hueco entre dos porciones estructurales de una aeronave
US9505485B2 (en) * 2012-05-08 2016-11-29 Lockheed Martin Corporation Vortex generation
GB201522486D0 (en) * 2015-12-21 2016-02-03 Airbus Operations Ltd Seal assembly
EP3318783A1 (en) * 2016-11-02 2018-05-09 Airbus Operations GmbH Fairing for an aircraft
GB2580930A (en) * 2019-01-30 2020-08-05 Airbus Operations Ltd Fairing for folding wing tip

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4705236A (en) * 1981-09-29 1987-11-10 The Boeing Company Aileron system for aircraft and method of operating the same
US4962902A (en) 1989-03-20 1990-10-16 The Boeing Company Aircraft control surface linkage
GB8919057D0 (en) * 1989-08-22 1989-10-04 British Aerospace Fairing arrangements for aircraft
GB8921749D0 (en) * 1989-09-27 1989-11-08 British Aerospace Fairing arrangements for aircraft
GB8924982D0 (en) 1989-11-06 1989-12-28 British Aerospace Fairing arrangement for aircraft
US5098043A (en) * 1990-02-27 1992-03-24 Grumman Aerospace Corporation Integrated power hinge actuator
US5388788A (en) 1993-12-16 1995-02-14 The Boeing Company Hinge fairings for control surfaces
US5915653A (en) * 1996-01-02 1999-06-29 The Boeing Company Spherical mating fairings for hingeline applications
GB2323576B (en) 1997-03-26 2001-08-22 British Aerospace Fairing arrangements for aircraft

Also Published As

Publication number Publication date
EP1206382A1 (en) 2002-05-22
WO2001015972A1 (en) 2001-03-08
ATE236044T1 (de) 2003-04-15
EP1206382B1 (en) 2003-04-02
AU6713000A (en) 2001-03-26
US6450457B1 (en) 2002-09-17
JP3655586B2 (ja) 2005-06-02
CA2382773C (en) 2008-11-18
GB9920318D0 (en) 1999-11-03
DE60001964T2 (de) 2003-11-06
CA2382773A1 (en) 2001-03-08
DE60001964D1 (de) 2003-05-08
JP2003508287A (ja) 2003-03-04

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