BRPI0506586A - guia de flape de aterrissagem para aeronave - Google Patents

guia de flape de aterrissagem para aeronave

Info

Publication number
BRPI0506586A
BRPI0506586A BRPI0506586-0A BRPI0506586A BRPI0506586A BR PI0506586 A BRPI0506586 A BR PI0506586A BR PI0506586 A BRPI0506586 A BR PI0506586A BR PI0506586 A BRPI0506586 A BR PI0506586A
Authority
BR
Brazil
Prior art keywords
landing flap
aircraft landing
guide
flap guide
aircraft
Prior art date
Application number
BRPI0506586-0A
Other languages
English (en)
Inventor
Rainer Gartelmann
Bodo Zapf
Knut Hachmann
Original Assignee
Airbus Gmbh
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 Gmbh filed Critical Airbus Gmbh
Publication of BRPI0506586A publication Critical patent/BRPI0506586A/pt

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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bearings For Parts Moving Linearly (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

GUIA DE FLAPE DE ATERRISSAGEM PAR AERONAVE A invenção propõe um guia de flape de aterrissagem para aeronave, em que o movimento do flape de aterrissagem de translação (1) é realizado com um cursor de planar (4) que é sustentado e guiado em deslizadores do transportador de flape de aterrissagem (3). o cursor(4) é conectado ao flape de aterrissagem (1) guiado ao longo do transportador de flape (3) por intermédio de pelo menos um guia de de planar (41,42,43,44).
BRPI0506586-0A 2004-02-12 2005-02-11 guia de flape de aterrissagem para aeronave BRPI0506586A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102004006940A DE102004006940B4 (de) 2004-02-12 2004-02-12 Landeklappenführung für Luftfahrzeuge
US60664604P 2004-09-02 2004-09-02
PCT/EP2005/001391 WO2005077756A1 (en) 2004-02-12 2005-02-11 Landing flap guide for aircraft

Publications (1)

Publication Number Publication Date
BRPI0506586A true BRPI0506586A (pt) 2007-05-02

Family

ID=34832624

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0506586-0A BRPI0506586A (pt) 2004-02-12 2005-02-11 guia de flape de aterrissagem para aeronave

Country Status (8)

Country Link
US (1) US7857263B2 (pt)
EP (1) EP1713688B1 (pt)
JP (1) JP4571953B2 (pt)
CN (1) CN1918033B (pt)
BR (1) BRPI0506586A (pt)
CA (1) CA2554067C (pt)
DE (1) DE102004006940B4 (pt)
WO (1) WO2005077756A1 (pt)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006036464B4 (de) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
GB0810460D0 (en) * 2008-06-09 2008-07-09 Airbus Uk Ltd Support assembly
GB0810584D0 (en) * 2008-06-11 2008-07-16 Airbus Uk Ltd Aircraft wing assembly
DE102009039967A1 (de) * 2009-09-03 2011-03-10 Airbus Operations Gmbh Verstellmechanismus zur kinematischen Führung eines Verstellkörpers bei dessen Verstellung an einem tragenden Strukturteil, Verstellmechanismus zur kinematischen Verstellung eines Hochauftriebskörpers sowie Hochauftriebssystem mit einem solchen Verstellmechanismus
US9359972B2 (en) 2011-08-31 2016-06-07 United Technologies Corporation Multi axis slide carriage system
DE102011082888B4 (de) * 2011-09-16 2016-01-07 Airbus Defence and Space GmbH Auftriebsklappenanordnung, Tragflügel sowie Flugzeug
GB201209686D0 (en) 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
WO2014209714A1 (en) * 2013-06-26 2014-12-31 Learjet Inc. Mechanism for trailing edge control surface
EP2942272A1 (en) 2014-05-09 2015-11-11 Airbus Operations GmbH An aircraft wing and an aircraft comprising such aircraft wing
EP3025955B1 (de) 2014-11-26 2019-06-19 Airbus Defence and Space GmbH Hochauftriebssystem
BE1024276B1 (fr) * 2016-11-04 2018-01-11 Sonaca Sa Aile d’aeronef comprenant un volet mobile de bord de fuite entraine par un moteur electrique lineaire
ES2878314T3 (es) 2017-04-26 2021-11-18 Asco Ind Nv Conjunto de guía para una pista portadora del dispositivo hipersustentador del borde delantero aerodinámico
US20190127047A1 (en) * 2017-10-30 2019-05-02 Airbus Operations Gmbh Carriage for supporting and guiding a flap and airfoil flap system for use in an aircraft
EP3501977B1 (en) 2017-12-19 2021-08-11 Asco Industries NV Deployment system for an airfoil high lift leading edge device
EP3878734B1 (en) * 2020-03-11 2023-07-19 Airbus Operations GmbH Guiding element for a high lift airfoil arrangement of an aircraft, high lift airfoil arrangement and production method
CN113697087B (zh) * 2021-08-13 2024-06-11 航天时代飞鹏有限公司 一种大型货运无人机着陆构型及其设计方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1075439B (de) * 1960-02-11 Societe de Brevets H.D., Paris Flugzeugtragfläche mit Klappen längs der Hinterkante zur Auftriebserhöhung
DE698114C (de) * 1938-03-26 1940-11-01 Dornier Werke Gmbh Rollfluegel
US3767140A (en) * 1971-11-03 1973-10-23 Mc Donnell Douglas Corp Airplane flaps
AT335101B (de) 1972-10-28 1977-02-25 Rensch Eberhard Bausatz zur montage von mobeln
DE2949293A1 (de) * 1979-12-07 1981-06-11 GRS Gesellschaft für Raketen-Systeme mbH, 5300 Bonn Klappleitwerk fuer durch raketentreibsaetze angetriebene flugkoerper
US4381093A (en) * 1980-10-07 1983-04-26 The Boeing Company Flap assembly for aircraft wing
DE3713465A1 (de) * 1987-04-22 1988-11-10 Messerschmitt Boelkow Blohm Tandem-landeklappenwagen
GB8718977D0 (en) 1987-08-11 1987-09-16 British Aerospace Trailing edge flaps
EP0460003B1 (de) * 1989-02-23 1993-05-12 ZF FRIEDRICHSHAFEN Aktiengesellschaft Antriebseinrichtung mit variablem drehmoment-begrenzungssystem
US5094412A (en) * 1989-10-13 1992-03-10 Bell Helicopter Textron Inc. Flaperon system for tilt rotor wings
DE4107556C1 (pt) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
RU2022879C1 (ru) 1991-04-09 1994-11-15 Авиационный научно-технический комплекс им.О.К.Антонова Носок крыла самолета
US5681013A (en) * 1995-12-26 1997-10-28 The Boeing Company Vortex leading edge flap assembly for supersonic airplanes
DE19732953C1 (de) * 1997-07-31 1999-03-11 Daimler Benz Ag Tragflügel mit Landeklappe
JP2001127969A (ja) 1999-10-26 2001-05-11 Canon Inc 画像通信装置
AT410656B (de) 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten

Also Published As

Publication number Publication date
EP1713688B1 (en) 2010-07-28
DE102004006940B4 (de) 2009-02-26
JP4571953B2 (ja) 2010-10-27
CA2554067A1 (en) 2005-08-25
JP2007522017A (ja) 2007-08-09
CN1918033B (zh) 2011-11-09
US20080042009A1 (en) 2008-02-21
CA2554067C (en) 2012-10-09
DE102004006940A1 (de) 2005-09-08
US7857263B2 (en) 2010-12-28
EP1713688A1 (en) 2006-10-25
WO2005077756A1 (en) 2005-08-25
CN1918033A (zh) 2007-02-21

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH

B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]

Free format text: INDEFIRO O PEDIDO DE ACORDO COM O(S) ARTIGO(S) 8O E 13 DA LPI

B09B Patent application refused [chapter 9.2 patent gazette]

Free format text: MANTIDO O INDEFERIMENTO UMA VEZ QUE NAO FOI APRESENTADO RECURSO DENTRO DO PRAZO LEGAL.