BR112015010210A2 - asa de avião, avião, sistema de flape para uma asa de avião, e, método para ajustar a posição de um flape de uma asa de avião - Google Patents

asa de avião, avião, sistema de flape para uma asa de avião, e, método para ajustar a posição de um flape de uma asa de avião

Info

Publication number
BR112015010210A2
BR112015010210A2 BR112015010210A BR112015010210A BR112015010210A2 BR 112015010210 A2 BR112015010210 A2 BR 112015010210A2 BR 112015010210 A BR112015010210 A BR 112015010210A BR 112015010210 A BR112015010210 A BR 112015010210A BR 112015010210 A2 BR112015010210 A2 BR 112015010210A2
Authority
BR
Brazil
Prior art keywords
flap
tracking member
wing
airplane
actuator
Prior art date
Application number
BR112015010210A
Other languages
English (en)
Other versions
BR112015010210B1 (pt
Inventor
Marinus Franciscus Bastiaansen Adrianus
Schoonhoven Michel
Original Assignee
Fokker Aerostructures Bv
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 Fokker Aerostructures Bv filed Critical Fokker Aerostructures Bv
Publication of BR112015010210A2 publication Critical patent/BR112015010210A2/pt
Publication of BR112015010210B1 publication Critical patent/BR112015010210B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • 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
    • 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

1 / 1 resumo “asa de aviãƒo, aviãƒo, sistema de flape para uma asa de aviãƒo, e, mã‰todo para ajustar a posiã‡ãƒo de um flape de uma asa de aviãƒo” uma asa de aviã£o compreende uma asa principal e um sistema de flape que tem um flape no bordo de fuga da asa principal. um membro de rastreamento do flape alongado ã© conectado na asa principal de uma maneira tal que pode ser movimentado substancialmente em sua direã§ã£o longitudinal e ã© guiado por elementos de mancal de suporte em relaã§ã£o ã  asa principal entre uma posiã§ã£o retraã­da para a frente e uma posiã§ã£o estendida para trã¡s. o flape ã© rotativamente conectado na extremidade traseira do membro de rastreamento do flape de uma maneira tal que ele pode girar em torno de um eixo geomã©trico de rotaã§ã£o que estende-se substancialmente paralelo ao bordo de fuga da asa principal, de forma que o flape move junto com o membro de rastreamento do flape quando o membro de rastreamento do flape ã© movimentado e de forma que o flape pode ser rotado em torno do eixo geomã©trico de rotaã§ã£o de forma mecanicamente independente do movimento do membro de rastreamento do flape. o sistema de flape compreende um sistema atuador com dois atuadores. o primeiro atuador ã© conectado na asa principal e tem um membro de engate que engata o flape ou o membro de rastreamento do flape para mover o flape junto com o membro de rastreamento do flape de forma que o membro de rastreamento do flape ã© mã³vel entre sua posiã§ã£o retraã­da e sua posiã§ã£o estendida. o segundo atuador ã© conectado no membro de rastreamento do flape de forma que o segundo atuador move junto com o membro de rastreamento do flape quando o membro de rastreamento do flape ã© movimentado por meio do primeiro atuador. o segundo atuador tem um membro de engate que engata o flape para rotar o flape em torno do eixo geomã©trico de rotaã§ã£o.
BR112015010210-7A 2012-11-06 2013-10-29 Sistema de flape para uma asa de avião, asa de avião, avião, e, método para ajustar a posição de um flape de uma asa de avião BR112015010210B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL2009762A NL2009762C2 (en) 2012-11-06 2012-11-06 An airplane wing, airplane and flap system.
NL2009762 2012-11-06
PCT/NL2013/050767 WO2014073954A1 (en) 2012-11-06 2013-10-29 An airplane wing, an airplane and a flap system

Publications (2)

Publication Number Publication Date
BR112015010210A2 true BR112015010210A2 (pt) 2017-07-11
BR112015010210B1 BR112015010210B1 (pt) 2020-12-15

Family

ID=47360262

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015010210-7A BR112015010210B1 (pt) 2012-11-06 2013-10-29 Sistema de flape para uma asa de avião, asa de avião, avião, e, método para ajustar a posição de um flape de uma asa de avião

Country Status (13)

Country Link
US (1) US9868512B2 (pt)
EP (1) EP2917101B1 (pt)
JP (1) JP2016501764A (pt)
KR (1) KR20150094623A (pt)
CN (1) CN104903191B (pt)
AU (1) AU2013341918A1 (pt)
BR (1) BR112015010210B1 (pt)
CA (1) CA2889873C (pt)
IL (1) IL238633A0 (pt)
MX (1) MX2015005606A (pt)
NL (1) NL2009762C2 (pt)
RU (1) RU2015118980A (pt)
WO (1) WO2014073954A1 (pt)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10279891B2 (en) * 2016-06-02 2019-05-07 Google Llc Software controlled stiffening of flexible aircraft
WO2018005534A1 (en) * 2016-06-30 2018-01-04 Bombardier Inc. Assemblies and methods for deploying a trailing edge flap of an aircraft
CN106353065B (zh) * 2016-09-12 2018-07-17 中国商用飞机有限责任公司 用于在风洞试验中调节襟翼的无级调节装置及飞机
EP3301017B1 (en) * 2016-09-30 2019-08-07 Airbus Operations GmbH System for driving and guiding of a trailing edge control surface
NL2018538B1 (en) * 2017-03-17 2018-09-24 Fokker Aerostructures Bv Airfoil-shaped body with a variable outer shape
EP3395679B1 (en) * 2017-04-28 2021-09-01 Airbus Operations GmbH Wing for an aircraft
US10766600B2 (en) * 2017-07-28 2020-09-08 The Boeing Company Articulation assemblies for retracting aircraft flap support fairings and related methods
US11046434B2 (en) * 2017-09-19 2021-06-29 The Boeing Company Methods and apparatus to align and secure aircraft
US10974816B2 (en) * 2017-09-28 2021-04-13 The Boeing Company High-fowler flap actuation apparatus and related methods
US10829203B2 (en) * 2018-04-06 2020-11-10 The Boeing Company Distributed trailing edge wing flap systems
US11338904B2 (en) * 2018-05-23 2022-05-24 Airbus Operations Gmbh Flight control surface assembly
US11192627B2 (en) * 2018-06-18 2021-12-07 Bombardier Inc. Aircraft wing with deployable flap
EP3584156A1 (en) 2018-06-20 2019-12-25 Bombardier Inc. Variable camber system
EP3584153A1 (en) * 2018-06-20 2019-12-25 Bombardier Inc. Variable camber system
CN109606638B (zh) * 2018-11-07 2022-05-27 中国航空工业集团公司西安飞机设计研究所 一种下沉铰链式襟翼摇臂支撑结构
CN109353489B (zh) * 2018-11-08 2020-08-14 浙江南洋科技股份有限公司 一种无人机多功能襟翼结构
EP3674202B1 (en) * 2018-12-28 2021-03-17 LEONARDO S.p.A. Aircraft wing
CN111003151A (zh) * 2019-12-24 2020-04-14 中国航空工业集团公司西安飞机设计研究所 一种上单翼通用飞机襟翼
CN112977798B (zh) * 2021-02-19 2022-10-11 湖北吉利太力飞车有限公司 一种机翼总成及飞行汽车
US20230192273A1 (en) * 2021-12-16 2023-06-22 Hamilton Sundstrand Corporation Aircraft control surface actuation mechanism
EP4234396A1 (en) * 2022-02-28 2023-08-30 Airbus Operations GmbH Wing for an aircraft
CN116639275B (zh) * 2023-05-18 2024-05-28 北京科技大学 一种扑翼飞行器编队方法

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2188083A (en) * 1937-03-11 1940-01-23 United Aircraft Corp Extendible slotted deflector flap
US2207453A (en) * 1937-10-02 1940-07-09 Arado Flugzeugwerke Gmbh Aircraft supporting wing
US2235146A (en) * 1938-06-22 1941-03-18 Harlan D Fowler Airplane
US2276688A (en) * 1938-11-28 1942-03-17 Dewoitine Emile Julien Eugene Control device for ailerons and flaps
DE748275C (de) * 1941-12-14 1944-10-30 Einrichtung zum Verstellen von Flugzeughilfstfluegeln
US2423984A (en) * 1943-07-12 1947-07-15 Lockheed Aircraft Corp Wing flap extending mechanism
US2609166A (en) * 1945-12-22 1952-09-02 Boeing Co Airplane flap supporting and control mechanism
US2620147A (en) * 1950-05-31 1952-12-02 Boeing Co Airplane flap control mechanism
US3583660A (en) * 1969-08-18 1971-06-08 Lockheed Aircraft Corp Lift and control augmenter for airfoils
US3655149A (en) * 1970-09-25 1972-04-11 Lockheed Aircraft Corp Flap actuating mechanism
JPS512198B1 (pt) * 1970-10-01 1976-01-23
US3853289A (en) * 1973-02-15 1974-12-10 Boeing Co Trailing edge flap and actuating mechanism therefor
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
US3985319A (en) * 1975-02-03 1976-10-12 The Boeing Company Variable pivot trailing edge flap
US4248395A (en) * 1975-03-24 1981-02-03 The Boeing Company Airplane wing trailing-edge flap-mounting mechanism
US4283029A (en) * 1979-01-02 1981-08-11 Rudolph Peter K C Actuating apparatus for a flap system having an upper surface blowing powered lift system
US4471928A (en) * 1980-08-13 1984-09-18 The Boeing Company Extendible airfoil track assembly
US4544118A (en) * 1982-09-30 1985-10-01 The Boeing Company Drive mechanism for combined flap-aileron surface
US5538202A (en) * 1993-11-02 1996-07-23 Northrop Grumman Corporation Hydraulic actuation system for aircraft control surfaces
US5788190A (en) * 1996-10-22 1998-08-04 The Boeing Company Slotted cruise trailing edge flap
DE19741326C2 (de) * 1997-09-19 2003-11-20 Deutsch Zentr Luft & Raumfahrt Anströmprofil mit variabler Profiladaption
US6598834B2 (en) * 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
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
GB0921007D0 (en) * 2009-11-30 2010-01-13 Airbus Operations Ltd Trailing edge flap

Also Published As

Publication number Publication date
CA2889873A1 (en) 2014-05-15
US9868512B2 (en) 2018-01-16
WO2014073954A1 (en) 2014-05-15
AU2013341918A1 (en) 2015-06-04
BR112015010210B1 (pt) 2020-12-15
JP2016501764A (ja) 2016-01-21
KR20150094623A (ko) 2015-08-19
EP2917101A1 (en) 2015-09-16
CN104903191A (zh) 2015-09-09
US20150291275A1 (en) 2015-10-15
IL238633A0 (en) 2015-06-30
MX2015005606A (es) 2015-11-06
CN104903191B (zh) 2017-03-15
EP2917101B1 (en) 2016-12-07
CA2889873C (en) 2019-03-12
NL2009762C2 (en) 2014-05-08
RU2015118980A (ru) 2016-12-27

Similar Documents

Publication Publication Date Title
BR112015010210A2 (pt) asa de avião, avião, sistema de flape para uma asa de avião, e, método para ajustar a posição de um flape de uma asa de avião
BRPI0811030A2 (pt) aeronave
JP2016501764A5 (pt)
GB0906952D0 (en) Aircraft assembly and spar
CY1122262T1 (el) Τουρμπινα καθετου αξονα
EP2730499A3 (en) Wing fold system
BR112012027644A2 (pt) unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave
WO2013000577A3 (en) Airfoil with a main wing and a high-lift body and method for realizing adjusting movements of a high-lift body relative to a main wing
BRPI0714773A2 (pt) Sistema de alta sustentação para uma aeronave
BR112012009226A2 (pt) bloco de batente do bogie
GB201117340D0 (en) Flat support
GB201317289D0 (en) System for changing the pitch of the contra-rotating propellers of a turboshaft engine
BR112012011240A2 (pt) maca de empurrar rolante , e, método de operação de uma maca de empurrar rolante
GB201018924D0 (en) Seal
BR112015012320A2 (pt) trava de balancim para controlar atuação de válvula de motor
BR112013018863A2 (pt) aeronave
BR112015006941A2 (pt) sistema de guia de acionamento de topo, e, método para montar um sistema de guia de acionamento de topo
BR112015030731A2 (pt) pá de rotor e usina de energia eólica
BR112015029704A2 (pt) estrutura de lâminas
BR112014032030A2 (pt) sistema de movimentação rotacional de um rastreador solar, e, dispositivo de rastreamento solar
BR112015018741A2 (pt) retentor de tanque em uma aeronave
JP2013002447A5 (pt)
BR112014005241A2 (pt) sistema de bomba, e, método para operar uma bomba
BR112013022291A2 (pt) método de operar de maneira simultânea atuadores para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivo
BR112014027734A2 (pt) unidade de propulsão rotativa

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 29/10/2013, OBSERVADAS AS CONDICOES LEGAIS.