BRPI0716819A2 - Elemento aerodinâmico e asa com elemento aerodinâmico, módulo atuador de ativação, computador, programa de computador e método para influenciar contracorrentes de rastro - Google Patents

Elemento aerodinâmico e asa com elemento aerodinâmico, módulo atuador de ativação, computador, programa de computador e método para influenciar contracorrentes de rastro

Info

Publication number
BRPI0716819A2
BRPI0716819A2 BRPI0716819-5A2A BRPI0716819A BRPI0716819A2 BR PI0716819 A2 BRPI0716819 A2 BR PI0716819A2 BR PI0716819 A BRPI0716819 A BR PI0716819A BR PI0716819 A2 BRPI0716819 A2 BR PI0716819A2
Authority
BR
Brazil
Prior art keywords
aerodynamic element
computer
countercurrents
wing
actuator module
Prior art date
Application number
BRPI0716819-5A2A
Other languages
English (en)
Inventor
Christian Breitsamter
Alexander Allen
Original Assignee
Airbus Gmbh
Univ Muenchen Tech
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, Univ Muenchen Tech filed Critical Airbus Gmbh
Publication of BRPI0716819A2 publication Critical patent/BRPI0716819A2/pt

Links

Classifications

    • 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
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/076—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. 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
    • Y02T50/10—Drag reduction
BRPI0716819-5A2A 2006-09-15 2007-09-15 Elemento aerodinâmico e asa com elemento aerodinâmico, módulo atuador de ativação, computador, programa de computador e método para influenciar contracorrentes de rastro BRPI0716819A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006043469 2006-09-15
PCT/EP2007/008038 WO2008031620A2 (de) 2006-09-15 2007-09-15 Aerodynamischer körper sowie tragflügel mit aerodynamischem körper, stellantriebs -ansteuermodul, computer, computerprogramm und verfahren zur beeinflussung von nachlauf wirbeln

Publications (1)

Publication Number Publication Date
BRPI0716819A2 true BRPI0716819A2 (pt) 2013-11-05

Family

ID=38814407

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0716819-5A2A BRPI0716819A2 (pt) 2006-09-15 2007-09-15 Elemento aerodinâmico e asa com elemento aerodinâmico, módulo atuador de ativação, computador, programa de computador e método para influenciar contracorrentes de rastro

Country Status (8)

Country Link
US (1) US8387922B2 (pt)
EP (1) EP2064116B1 (pt)
JP (1) JP2010503571A (pt)
CN (1) CN101535125B (pt)
BR (1) BRPI0716819A2 (pt)
CA (1) CA2663437A1 (pt)
RU (1) RU2009113854A (pt)
WO (1) WO2008031620A2 (pt)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
WO2009155584A1 (en) 2008-06-20 2009-12-23 Aviation Partners, Inc. Curved wing tip
DE102009001251A1 (de) * 2009-03-01 2010-09-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Tragflügel für ein Flugzeug mit einem Winglet an der Flügelspitze
EP2233395A1 (en) 2009-03-24 2010-09-29 EADS Deutschland GmbH Winglet with autonomously actuated tab
US8389293B2 (en) * 2009-11-17 2013-03-05 Abbott Point Of Care Inc. Reducing leukocyte interference in competitive immunoassays
US20110127383A1 (en) 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
CA2783401A1 (en) * 2009-12-10 2011-06-16 University Of The Witwatersrand, Johannesburg Method for reducing in flight wake vortices and an aircraft wingtip arrangement used in such method
US8476079B2 (en) 2010-04-30 2013-07-02 Abbott Point Of Care Inc. Reagents for reducing leukocyte interference in immunoassays
US8394325B2 (en) 2010-06-14 2013-03-12 Abbott Point Of Care Inc. Magnetic beads for reducing leukocyte interference in immunoassays
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
CN106081070A (zh) * 2011-06-09 2016-11-09 航空伙伴股份有限公司 螺旋形机翼末梢以及飞行器
EP2834146B1 (en) * 2012-04-03 2023-10-11 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
US9567066B2 (en) 2013-02-05 2017-02-14 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
EP2998218A1 (en) * 2014-09-16 2016-03-23 Airbus Operations GmbH A wing for an aircraft, and an aircraft comprising such a wing
CN104895876B (zh) * 2015-05-22 2018-01-16 厦门大学 一种基于径向不稳定性的加速漩涡破裂的方法
EP3269635A1 (en) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Airplane wing
US10137999B2 (en) * 2017-03-30 2018-11-27 The Boeing Company Methods and apparatus for detecting airflow control surface skew conditions
CN108116658B (zh) * 2017-12-13 2020-04-10 哈尔滨工业大学深圳研究生院 飞行器的控制方法、系统和飞行器
EP3511243B1 (en) * 2018-01-15 2021-12-29 The Aircraft Performance Company GmbH Airplane wing
US11897601B2 (en) * 2022-02-16 2024-02-13 Jetzero, Inc. Aircraft and methods of use for aerodynamic control with winglet surfaces

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2418301A (en) * 1942-07-24 1947-04-01 Miles Aircraft Ltd Aircraft supporting surface
US3174030A (en) * 1953-05-29 1965-03-16 Sperry Rand Corp Device for predicting values of a fluctuating system at a predetermined future time
US2846165A (en) * 1956-06-25 1958-08-05 John A Axelson Aircraft control system
GB850249A (en) 1958-11-11 1960-10-05 Westinghouse Electric Corp Improvements in or relating to aircraft control systems
US3462662A (en) 1967-04-12 1969-08-19 Lear Siegler Inc Monitoring and fault correction system for a multiple channel servo actuator
US3561326A (en) * 1968-03-06 1971-02-09 Parker Hannifin Corp Pulse phase modulated servoactuator
DE2149956C3 (de) * 1971-10-07 1974-03-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochauftriebsflügel
GB1435489A (en) * 1972-08-02 1976-05-12 Emi Ltd Automatic vehicle guidance systems
US3981460A (en) * 1973-08-30 1976-09-21 Robert N. Starr Staggered channel wing-type aircraft
US4197655A (en) * 1977-11-09 1980-04-15 Cessna Aircraft Company Gyroscopic method and apparatus for determining magnetic heading and attitude
FR2591557B1 (fr) * 1985-12-13 1988-03-25 Aerospatiale Systeme de couplage de deux volets d'une aile d'aeronef, et aile d'aeronef equipee d'un tel systeme
CN1114944A (zh) * 1994-07-12 1996-01-17 傅前哨 在翼尖部安装叶轮的飞机机翼
KR0179115B1 (ko) 1995-11-20 1999-05-01 구자홍 액정배향용 감광성물질 및 이를 이용한 액정표시장치
US6082679A (en) 1997-06-26 2000-07-04 The Boeing Company Active system for early destruction of trailing vortices
US5988563A (en) * 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
FR2841211B1 (fr) * 2002-06-21 2004-12-17 Airbus France Procede et dispositif pour reduire les mouvements vibratoires du fuselage d'un aeronef
DE20211664U1 (de) * 2002-07-29 2003-01-09 Kaehler Kai Seitenruder-Anordnung
US7770842B2 (en) * 2004-08-24 2010-08-10 Honeywell International Inc. Aircraft flight control surface actuation system communication architecture
US8380364B2 (en) * 2006-05-17 2013-02-19 Textron Innovations, Inc. Manual and computerized flight control system with natural feedback
JP4657191B2 (ja) * 2006-11-02 2011-03-23 本田技研工業株式会社 飛行機の主翼構造

Also Published As

Publication number Publication date
CN101535125B (zh) 2013-06-19
EP2064116A2 (de) 2009-06-03
CN101535125A (zh) 2009-09-16
CA2663437A1 (en) 2008-03-20
US8387922B2 (en) 2013-03-05
RU2009113854A (ru) 2010-10-20
WO2008031620A3 (de) 2008-05-08
EP2064116B1 (de) 2014-07-23
JP2010503571A (ja) 2010-02-04
WO2008031620A2 (de) 2008-03-20
US20100006706A1 (en) 2010-01-14

Similar Documents

Publication Publication Date Title
BRPI0716819A2 (pt) Elemento aerodinâmico e asa com elemento aerodinâmico, módulo atuador de ativação, computador, programa de computador e método para influenciar contracorrentes de rastro
BR112012001288A2 (pt) métodos implementado por computador para proporcionar a aplicativo de navegador acesso a informações associadas a parte de sistema de arquivo e produtos de programa de computador
BRPI0810084A2 (pt) Sistema eletrônico para influenciar funções celulares em um indivíduo mamífero de sangue quente
FI20060858A0 (fi) Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
BRPI0915207A2 (pt) dispositivo para formação de vórtices aerodinâmicos, bem como flape de regulagem e asa de sustentação com um dispositivo para formação de vórtices aerodinâmicos
FI20086259A0 (fi) Kaksitoiminen säätöelin rannetietokoneelle tai vastaavalle ja menetelmä rannetietokoneen tai vastaavan päätelaitteen säätämiseksi
DK2132441T3 (da) Vindenergianlæg med belastningsoverførerende konstruktionsdele
JP2011504149A5 (ja) 航空機翼の後縁フラップを移動させるための装置及び同装置を備えた航空機
BRPI0914968A2 (pt) veiculo pessoal para voo incluindo sistema de controle
BRPI0914270A2 (pt) duto de ar para fornecer ar ambiente em uma aeronave, e, método para operar o mesmo
BRPI0813734A2 (pt) Sistema informatizado de viagem, método em um sistema de viagem e programa de computador
BRPI0811086A2 (pt) Método e sistema para fabricação de um cartão de interface eletrônica e um cartão fabricado usando os mesmos
BRPI0919572A2 (pt) método implementado por computador em múltipla escala, sistema implementado por computador, e, método para operar um reservatório de subsuperfície
BRPI0722259A2 (pt) Método para produção de um vestuário absorvente, e vestuário absorvente produzido de acordo com o método
BRPI0717068A2 (pt) instruÇço e làgica para processar cadeias de texto.
DE602007006424D1 (de) Datenbus-schnittstelle mit unterbrechbarer uhr
FR2919267B1 (fr) Avion a signature acoustique reduite
BRPI0810971A2 (pt) Método de controle do arraste de particulados por fluidos e composição de lodo aquoso do método
BRPI0915404A2 (pt) gotículas microfluídicas para engenharia metabólica e outras aplicações
DE502007003917D1 (de) Querträger, insbesondere ein Cockpitquerträger
BRPI0820703A2 (pt) Algoritimos rápidos para computação de dct-ii de 5-pontos, dct-iv, e dst-iv, e arquiteturas
BRPI0920736A2 (pt) módulo de placa e método de fabricação do mesmo.
BRPI0907873A2 (pt) Elemento estrutural de absorção de energia feito de um material compósito e fuselagem de aeronave tendo o referido absorvedor
BRPI0820078A2 (pt) Sistema e método para a marcação de quaisquer objetos, vivos ou não, bem como elemento de marcação e utilização deste para a marcação de quaisquer objetos, em especial para o controle de objetos e para a administração de objetos
BRPI0821427A2 (pt) Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião.

Legal Events

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

Owner name: TECHNISCHE UNIVERSITAET MUENCHEN (DE) , AIRBUS OPE

B08L Patent application lapsed because of non payment of annual fee [chapter 8.12 patent gazette]

Free format text: REFERENTE AO NAO RECOLHIMENTO DAS 6A E 7A ANUIDADES.

B08I Publication cancelled [chapter 8.9 patent gazette]

Free format text: ANULADA A PUBLICACAO CODIGO 8.12 NA RPI NO 2277 DE 26/08/2014 POR TER SIDO INDEVIDA.

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 6A, 7A, 8A, 9A, 10A, 11A, 12A E 13A ANUIDADES.

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 2602 DE 17-11-2020 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.