BRPI0506586A - guia de flape de aterrissagem para aeronave - Google Patents
guia de flape de aterrissagem para aeronaveInfo
- 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
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).
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)
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 |
EP3395678B1 (en) | 2017-04-26 | 2021-05-26 | Asco Industries NV | Guidance assembly for an airfoil leading edge high-lift device carrier track |
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 |
ES2886667T3 (es) | 2017-12-19 | 2021-12-20 | Asco Ind Nv | Sistema de despliegue para un dispositivo de borde de ataque de sustentación elevada de perfil aerodinámico |
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)
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 |
DE59001450D1 (de) * | 1989-02-23 | 1993-06-17 | Zahnradfabrik Friedrichshafen | 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 |
-
2004
- 2004-02-12 DE DE102004006940A patent/DE102004006940B4/de not_active Expired - Fee Related
-
2005
- 2005-02-11 WO PCT/EP2005/001391 patent/WO2005077756A1/en active Application Filing
- 2005-02-11 EP EP05707337A patent/EP1713688B1/en not_active Not-in-force
- 2005-02-11 JP JP2006552558A patent/JP4571953B2/ja not_active Expired - Fee Related
- 2005-02-11 US US10/589,120 patent/US7857263B2/en not_active Expired - Fee Related
- 2005-02-11 BR BRPI0506586-0A patent/BRPI0506586A/pt not_active Application Discontinuation
- 2005-02-11 CA CA2554067A patent/CA2554067C/en not_active Expired - Fee Related
- 2005-02-11 CN CN2005800047581A patent/CN1918033B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN1918033B (zh) | 2011-11-09 |
DE102004006940A1 (de) | 2005-09-08 |
JP2007522017A (ja) | 2007-08-09 |
JP4571953B2 (ja) | 2010-10-27 |
WO2005077756A1 (en) | 2005-08-25 |
CA2554067A1 (en) | 2005-08-25 |
EP1713688B1 (en) | 2010-07-28 |
EP1713688A1 (en) | 2006-10-25 |
US20080042009A1 (en) | 2008-02-21 |
US7857263B2 (en) | 2010-12-28 |
CA2554067C (en) | 2012-10-09 |
DE102004006940B4 (de) | 2009-02-26 |
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. |