BRPI0507038A - flap móvel de borda de ataque de uma asa principal do velame de uma aeronave, e, asa principal do velame de uma aeronave - Google Patents

flap móvel de borda de ataque de uma asa principal do velame de uma aeronave, e, asa principal do velame de uma aeronave

Info

Publication number
BRPI0507038A
BRPI0507038A BRPI0507038-4A BRPI0507038A BRPI0507038A BR PI0507038 A BRPI0507038 A BR PI0507038A BR PI0507038 A BRPI0507038 A BR PI0507038A BR PI0507038 A BRPI0507038 A BR PI0507038A
Authority
BR
Brazil
Prior art keywords
main wing
flap
leading edge
canopy main
aircraft canopy
Prior art date
Application number
BRPI0507038-4A
Other languages
English (en)
Inventor
Chistian Overbergh
Michel Hautecoeur
Original Assignee
Sonaca Sa
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 Sonaca Sa filed Critical Sonaca Sa
Publication of BRPI0507038A publication Critical patent/BRPI0507038A/pt
Publication of BRPI0507038B1 publication Critical patent/BRPI0507038B1/pt
Publication of BRPI0507038B8 publication Critical patent/BRPI0507038B8/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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • 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)
  • Catching Or Destruction (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)

Abstract

FLAP MóVEL DE BORDA DE ATAQUE DE UMA ASA PRINCIPAL DO VELAME DE UMA AERONAVE, E, ASA PRINCIPAL DO VELAME DE UMA AERONAVE A invenção se refere a um flap móvel de borda de ataque (16) de uma asa principal de aeronave (1), esse flap compreendendo um revestimento aerodinâmico (18) que apresenta uma zona frontal sensível aos impactos de aves (24), assim como um revestimento traseiro (28) solidário do revestimento aerodinâmico (18), o flap compreendendo também uma pluraridade de nervuras (34) espaçadas ao longo de um direção longitudinal de borda de ataque (X'). De acordo com a imvenção, o flap compreende por outro lado, entre duas nervuras diratamente consecutivas, uma única parede rígida de desvio de trajetória de ave (42) montada fixamrnte nos revestimentos (18,28). Por outro lado, en seção tomada de acordo com um plano ortogonal à direção (X'), a parede (42) forma com uma corda geométrica (26) do flap um ângulo (<244>1) de um valor inferior 45<198>.
BRPI0507038A 2004-01-22 2005-01-20 flap móvel de borda de ataque de uma asa principal do velame de uma aeronave, e, asa principal do velame de uma aeronave BRPI0507038B8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
BE2004/0037 2004-01-22
BE2004/0037A BE1015867A3 (fr) 2004-01-22 2004-01-22 Ensemble de bord d'attaque d'un element de voilure d'aeronef et element de voilure equipee d'au moins un tel ensemble.
PCT/EP2005/050226 WO2005070762A1 (fr) 2004-01-22 2005-01-20 Volet mobile de bord d'attaque d'une aile principale de la voilure d'un aeronef, et aile principale munie d'un tel volet

Publications (3)

Publication Number Publication Date
BRPI0507038A true BRPI0507038A (pt) 2007-06-05
BRPI0507038B1 BRPI0507038B1 (pt) 2018-03-06
BRPI0507038B8 BRPI0507038B8 (pt) 2018-12-11

Family

ID=34800133

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0507038A BRPI0507038B8 (pt) 2004-01-22 2005-01-20 flap móvel de borda de ataque de uma asa principal do velame de uma aeronave, e, asa principal do velame de uma aeronave

Country Status (10)

Country Link
US (1) US7731128B2 (pt)
EP (1) EP1706315B1 (pt)
JP (1) JP4531066B2 (pt)
AT (1) ATE393728T1 (pt)
BE (1) BE1015867A3 (pt)
BR (1) BRPI0507038B8 (pt)
CA (1) CA2553701C (pt)
DE (1) DE602005006384T2 (pt)
ES (1) ES2306081T3 (pt)
WO (1) WO2005070762A1 (pt)

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DE602006013236D1 (de) * 2005-08-25 2010-05-12 Gkn Aerospace Services Ltd Vorflügel für eine Flugzeugtragfläche
DE102005060958A1 (de) * 2005-12-20 2007-06-21 Airbus Deutschland Gmbh Schutzvorrichtung
GB0604026D0 (en) * 2006-02-28 2006-04-12 Airbus Uk Ltd Aircraft wing
ES2315108B1 (es) * 2006-06-30 2010-01-12 Aibus España, S.L. Sistema de fijacion de un borde de ataque a la estructura de un plano sustentador de un avion.
US7753313B1 (en) * 2006-09-19 2010-07-13 The Boeing Company Composite wing slat for aircraft
JP4699487B2 (ja) * 2007-05-25 2011-06-08 三菱重工業株式会社 高揚力発生装置、翼および高揚力発生装置の騒音低減構造
MY152951A (en) 2009-06-30 2014-12-15 Sanofi Sa Solid pharmaceutical fixed dose compositions comprising irbesartan and amlodipine, their preparation and their therapeutic application
US9394046B2 (en) 2011-11-16 2016-07-19 Ecological Energy Company Fluid interface device as well as apparati and methods including same
CN103466078A (zh) * 2013-08-23 2013-12-25 中国航空工业集团公司西安飞机设计研究所 一种整体可拆卸式缝翼尾缘结构
EP2886449A1 (en) * 2013-12-23 2015-06-24 Airbus Operations S.L. Leading edge for an aircraft lifting surface
DE102014106743B4 (de) * 2014-05-13 2023-12-21 Airbus Operations Gmbh Strömungskörper mit einem darin integrierten Lasteinleitungselement, Verfahren zum Herstellen eines Strömungskörpers und Flugzeug mit einem solchen Strömungskörper
EP3204292B1 (en) * 2014-10-08 2020-01-15 Salver S.p.A. Process for assembling aircraft control surfaces
CN106986003B (zh) * 2017-03-15 2019-09-24 西北工业大学 一种有单斜板的抗鸟撞飞机尾翼前缘
GB201821332D0 (en) * 2018-12-31 2019-02-13 Airbus Operations Gmbh Aircraft flow body
ES2932841T3 (es) * 2019-01-18 2023-01-26 Asco Ind Nv Hipersustentador para un ala de aeronave, método para fabricar dicho hipersustentador
US11383821B2 (en) 2019-03-22 2022-07-12 Airbus Operations Gmbh Wing leading-edge device and a wing having such a wing leading-edge device
DE102019110948A1 (de) * 2019-04-29 2020-10-29 Airbus Operations Gmbh Vorderkanten-Bauteil für ein Flugzeug
US11230365B2 (en) * 2019-04-29 2022-01-25 Airbus Operations Gmbh Leading-edge component for an aircraft
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods
CN110304237B (zh) * 2019-07-15 2023-08-25 中国商用飞机有限责任公司 飞行器机翼及包括该飞行器机翼的飞行器
CN112124560B (zh) * 2020-09-18 2022-05-13 中国商用飞机有限责任公司 一种飞机翼的前缘结构
CN114476020B (zh) * 2021-12-20 2024-01-16 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种机翼用增升装置及飞机
CN115593613B (zh) * 2022-11-02 2023-08-15 江苏新扬新材料股份有限公司 一种轻量化抗鸟撞飞机平尾前缘

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US1956823A (en) * 1929-06-13 1934-05-01 Cairns Dev Company Wing structure
US2324303A (en) * 1941-02-25 1943-07-13 Lockheed Aircraft Corp Airplane antiicing construction
US4671471A (en) * 1984-05-21 1987-06-09 Mitchell Wing, Inc. Foam reinforced aluminum wing structure
DE3832949A1 (de) * 1988-09-28 1990-04-05 Claudius Dornier Seastar Gmbh Angestroemtes bauteil von flugkoerpern
US5484221A (en) * 1994-03-07 1996-01-16 Rockwell International Corp. Panel mounting system
US6315395B1 (en) * 1994-07-29 2001-11-13 Riso Kagaku Corporation Ink jet apparatus and conductive ink mixture
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WO1996036532A1 (en) * 1995-05-19 1996-11-21 Mcdonnell Douglas Corporation Airfoil lift management device
GB2324351A (en) * 1997-04-18 1998-10-21 British Aerospace Reducing drag in aircraft wing assembly
FR2783885B1 (fr) * 1998-09-25 2001-07-27 Geco As Structure portante a tourbillon marginal reduit
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ES2197727B1 (es) 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
JP4057331B2 (ja) * 2002-04-05 2008-03-05 日本飛行機株式会社 衝撃耐久構造体

Also Published As

Publication number Publication date
DE602005006384D1 (de) 2008-06-12
DE602005006384T2 (de) 2009-05-20
JP4531066B2 (ja) 2010-08-25
WO2005070762A1 (fr) 2005-08-04
ES2306081T3 (es) 2008-11-01
US7731128B2 (en) 2010-06-08
JP2007518626A (ja) 2007-07-12
ATE393728T1 (de) 2008-05-15
BRPI0507038B8 (pt) 2018-12-11
BRPI0507038B1 (pt) 2018-03-06
EP1706315B1 (fr) 2008-04-30
CA2553701A1 (en) 2005-08-04
BE1015867A3 (fr) 2005-10-04
CA2553701C (en) 2012-05-29
US20080237401A1 (en) 2008-10-02
EP1706315A1 (fr) 2006-10-04

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Legal Events

Date Code Title Description
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]
B16C Correction of notification of the grant [chapter 16.3 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 06/03/2018, OBSERVADAS AS CONDICOES LEGAIS. (CO) REFERENTE A RPI 2461 DE 06/03/2018, QUANTO AO NOME DO INVENTOR.