BR112012010496A2 - estrutura de movimento composto, aerofólio, estrutura de suporte e indução de movimento composto e aparelho. - Google Patents

estrutura de movimento composto, aerofólio, estrutura de suporte e indução de movimento composto e aparelho.

Info

Publication number
BR112012010496A2
BR112012010496A2 BR112012010496A BR112012010496A BR112012010496A2 BR 112012010496 A2 BR112012010496 A2 BR 112012010496A2 BR 112012010496 A BR112012010496 A BR 112012010496A BR 112012010496 A BR112012010496 A BR 112012010496A BR 112012010496 A2 BR112012010496 A2 BR 112012010496A2
Authority
BR
Brazil
Prior art keywords
composite motion
arm
airfoil
coupled
induction
Prior art date
Application number
BR112012010496A
Other languages
English (en)
Inventor
John Mcmurray Clark
Original Assignee
John Mcmurray Clark
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 John Mcmurray Clark filed Critical John Mcmurray Clark
Publication of BR112012010496A2 publication Critical patent/BR112012010496A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H21/00—Gearings comprising primarily only links or levers, with or without slides
    • F16H21/02—Gearings comprising primarily only links or levers, with or without slides the movements of two or more independently-moving members being combined into a single movement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
    • 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
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/18—Mechanical movements
    • Y10T74/18856—Oscillating to oscillating

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)
  • Manipulator (AREA)
  • Tires In General (AREA)
  • Automation & Control Theory (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Air-Flow Control Members (AREA)

Abstract

estrutura de movimento composto, aerofólio, estrutura de suporte e indução de movimento composto e aparlho uma estrutura de movimeno composto (3) para conexão entre duas superfícies compreendendo um primeiro braço (5) e um segundo braço (7) osciláveis acoplados juntos através de uma primeira conexão articulada (13), uma primeira superfície (35) acoplados acoplada em uma extremidade oposta do primeiro braço via uma segunda conexão articulada, uma segunda superfície (39) acoplado acoplada a uma extremidade oposta do segundo braço via uma terceira conexão articulada, o primeiro braço (5) e o segundo braço (7) sendo móveis, resultando, assim, em um movimento composto de uma ou ambas as superfícies.
BR112012010496A 2009-11-04 2010-11-04 estrutura de movimento composto, aerofólio, estrutura de suporte e indução de movimento composto e aparelho. BR112012010496A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US25799309P 2009-11-04 2009-11-04
US40140310P 2010-08-12 2010-08-12
PCT/AU2010/001473 WO2011054047A1 (en) 2009-11-04 2010-11-04 A compound motion structure

Publications (1)

Publication Number Publication Date
BR112012010496A2 true BR112012010496A2 (pt) 2016-03-15

Family

ID=43969484

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012010496A BR112012010496A2 (pt) 2009-11-04 2010-11-04 estrutura de movimento composto, aerofólio, estrutura de suporte e indução de movimento composto e aparelho.

Country Status (9)

Country Link
US (2) US9205912B2 (pt)
EP (1) EP2496473B1 (pt)
JP (1) JP5865840B2 (pt)
KR (1) KR20120091296A (pt)
CN (1) CN102741120B (pt)
AU (1) AU2010314745B2 (pt)
BR (1) BR112012010496A2 (pt)
CA (1) CA2816475A1 (pt)
WO (1) WO2011054047A1 (pt)

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GB201120992D0 (en) * 2011-12-07 2012-01-18 Airbus Uk Ltd Aircraft rib assembly
CN102645677B (zh) * 2012-05-14 2014-09-03 四川大学 金属圆环和条形卡槽组成的无扭动复摆
GB201222308D0 (en) 2012-12-11 2013-01-23 Airbus Operations Ltd Support assembly
GB2524050A (en) * 2014-03-12 2015-09-16 Airbus Operations Ltd An improved aerodynamic device
US10589837B2 (en) * 2016-02-08 2020-03-17 Bell Helicopter Textron Inc. Spar for a composite wing structure
EP3231702B1 (en) 2016-04-11 2020-06-17 Asco Industries NV High-lift device
EP3339164A1 (en) * 2016-12-22 2018-06-27 Airbus Operations GmbH Wing for an aircraft
US10683076B2 (en) 2017-10-31 2020-06-16 Coflow Jet, LLC Fluid systems that include a co-flow jet
CN108033012A (zh) * 2017-12-13 2018-05-15 四川宝天智控系统有限公司 Vtol固定翼无人机及其固定翼结构
US11920617B2 (en) 2019-07-23 2024-03-05 Coflow Jet, LLC Fluid systems and methods that address flow separation
US11292581B2 (en) * 2019-09-26 2022-04-05 Joby Aero Inc. Three-dimensional extension linkage
WO2021257271A1 (en) * 2020-06-17 2021-12-23 Coflow Jet, LLC Fluid systems having a variable configuration
WO2022204278A1 (en) 2021-03-26 2022-09-29 Coflow Jet, LLC Wind turbine blades and wind turbine systems that include a co-flow jet
CN114275142B (zh) * 2022-01-13 2023-08-25 北京机电工程研究所 一种连续变后缘弯度翼面

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US2218114A (en) * 1938-04-04 1940-10-15 Messerschmitt Boelkow Blohm Operating mechanism for aircraft wing flaps
FR858073A (fr) * 1939-04-18 1940-11-16 Perfectionnements apportés aux surfaces sustentatrices pour aérodynes
US2973925A (en) * 1958-03-24 1961-03-07 Lockheed Aircraft Corp Aerodynamically automatic airfoil slat mechanism
US3321238A (en) * 1965-08-23 1967-05-23 Gen Motors Corp Convertible vehicle body
DE2114670A1 (de) * 1971-03-26 1972-10-05 Vereinigte Flugtechnische Werke-Fokker GmbH, 2800 Bremen Vorrichtung zum Ausfahren eines Vorflügels aus Tragflächen von Luftfahrzeugen
US4180222A (en) * 1976-12-27 1979-12-25 Lockheed Aircraft Corporation Aileron segment control for a flaperon system
DE3013774A1 (de) * 1980-04-10 1981-10-15 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Betaetigungsanordnung fuer fluegelklappen
DE4107556C1 (pt) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5651513A (en) * 1995-03-01 1997-07-29 Northrop Grumman Corporation Linear flap drive system
US6010097A (en) * 1997-10-16 2000-01-04 Northrop Grumman Corporation Scissor linkage type slotted flap mechanism
US6481667B1 (en) * 2001-03-05 2002-11-19 Northrop Grumman Corporation System and method for deflecting an aerodynamic control surface
US6467733B1 (en) * 2001-11-28 2002-10-22 Northrop Grumman Corporation Aerodynamic control surface system
WO2003013956A1 (en) * 2002-03-21 2003-02-20 Nilesh Shriram Narvekar Flap deployment mechanism with swing arms
DE10328717B3 (de) * 2003-06-25 2004-12-02 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
DE102005044549B4 (de) * 2005-09-17 2008-04-17 Eads Deutschland Gmbh Flugzeugflügel mit ausfahrbarer Nasenklappe
US8104710B2 (en) * 2007-04-25 2012-01-31 Goodrich Actuation Systems Limited Actuator arrangement
GB0803692D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
CN101249889A (zh) * 2008-03-29 2008-08-27 王志成 飞行器用平板叶片推力装置
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Also Published As

Publication number Publication date
CA2816475A1 (en) 2011-05-12
RU2012121947A (ru) 2013-12-10
CN102741120A (zh) 2012-10-17
US20160097441A1 (en) 2016-04-07
AU2010314745A1 (en) 2012-06-21
JP5865840B2 (ja) 2016-02-17
EP2496473A4 (en) 2017-11-01
WO2011054047A1 (en) 2011-05-12
CN102741120B (zh) 2015-11-25
JP2013510747A (ja) 2013-03-28
EP2496473B1 (en) 2020-09-30
KR20120091296A (ko) 2012-08-17
US9205912B2 (en) 2015-12-08
US20120224964A1 (en) 2012-09-06
AU2010314745B2 (en) 2016-08-11
EP2496473A1 (en) 2012-09-12

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 9A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2538 DE 27-08-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.