BRPI0607925A2 - flap com fenda única com flap defletor deslizante e spoiler abaixável - Google Patents

flap com fenda única com flap defletor deslizante e spoiler abaixável

Info

Publication number
BRPI0607925A2
BRPI0607925A2 BRPI0607925-3A BRPI0607925A BRPI0607925A2 BR PI0607925 A2 BRPI0607925 A2 BR PI0607925A2 BR PI0607925 A BRPI0607925 A BR PI0607925A BR PI0607925 A2 BRPI0607925 A2 BR PI0607925A2
Authority
BR
Brazil
Prior art keywords
flap
spoiler
lowering
sliding deflector
single slotted
Prior art date
Application number
BRPI0607925-3A
Other languages
English (en)
Inventor
Klaus Bender
Ole Boettger
Original Assignee
Airbus Gmbh
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 filed Critical Airbus Gmbh
Publication of BRPI0607925A2 publication Critical patent/BRPI0607925A2/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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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
    • 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
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
  • Mechanical Control Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

FLAP COM FENDA úNICA COM FLAP DEFLETOR DESLIZANTE E SPOILER ABAIXáVEL. A presente invenção refere-se a um dispositivo para ajustar as características de sustentação de uma aeronave com um dispositivo de alta sustentação (2) que é fixado de modo móvel a um elemento de asa (1) e que compreende pelo menos um dispositivo de cobertura de fenda (3; 4), em que op pelo menos um dispositivo de cobertura de fenda (3; 4) é fixado de modo móvel no elemento de asa (1) O dispositivo de cobertura de fenda (3; 4) é designado para regular o tamanho de uma fenda (7) entre o elemento de asa (1) e o dispositivo de alta sustentação (2)
BRPI0607925-3A 2005-04-11 2006-04-07 flap com fenda única com flap defletor deslizante e spoiler abaixável BRPI0607925A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US67020105P 2005-04-11 2005-04-11
DE102005016578A DE102005016578A1 (de) 2005-04-11 2005-04-11 Einfachspaltklappe mit gleitender Abweiserklappe und absenkbarem Spoiler
PCT/EP2006/003212 WO2006108579A1 (en) 2005-04-11 2006-04-07 Single slotted flap with sliding deflector flap and lowerable spoiler

Publications (1)

Publication Number Publication Date
BRPI0607925A2 true BRPI0607925A2 (pt) 2009-10-20

Family

ID=37055256

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0607925-3A BRPI0607925A2 (pt) 2005-04-11 2006-04-07 flap com fenda única com flap defletor deslizante e spoiler abaixável

Country Status (9)

Country Link
US (1) US8066228B2 (pt)
EP (1) EP1868887B1 (pt)
JP (1) JP5185105B2 (pt)
CN (1) CN101155726B (pt)
BR (1) BRPI0607925A2 (pt)
CA (1) CA2598419C (pt)
DE (2) DE102005016578A1 (pt)
RU (1) RU2399553C2 (pt)
WO (1) WO2006108579A1 (pt)

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DE102006053259A1 (de) * 2006-11-11 2008-05-21 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs und Verfahren zu seiner Betätigung
US7874524B2 (en) * 2007-11-16 2011-01-25 The Boeing Company Methods and apparatus for a multi-segment flap fence
FR2929724B1 (fr) * 2008-04-02 2010-04-30 Airbus France Procede pour la determination de la vitesse de sortie d'effet de sol d'un aeronef.
GB0810724D0 (en) * 2008-06-12 2008-07-16 Airbus Uk Ltd Slat assembly
DE102008033005A1 (de) * 2008-07-14 2010-03-18 Airbus Deutschland Gmbh Aerodynamische Klappe und Flügel
US8424810B1 (en) 2010-03-31 2013-04-23 The Boeing Company Low noise wing slat system with rigid cove-filled slat
US8276852B2 (en) 2010-03-31 2012-10-02 The Boeing Company Low noise wing slat system with deployable wing leading edge elements
US8864083B1 (en) 2010-03-31 2014-10-21 The Boeing Company Low noise wing slat system with a fixed wing leading edge and deployable bridging panels
GB201117340D0 (en) * 2011-10-07 2011-11-23 Airbus Uk Ltd Flat support
GB2512318A (en) * 2013-03-26 2014-10-01 Eads Uk Ltd Lift-reducing apparatus for aircraft wings
US10000274B2 (en) * 2015-08-20 2018-06-19 The Boeing Company Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft
US11046425B2 (en) * 2016-05-20 2021-06-29 Bombardier Inc. Apparatus and methods for actuating a double-slotted flap using a slave screw
CN108100223A (zh) * 2017-11-29 2018-06-01 中国航空工业集团公司西安飞机设计研究所 一种涡桨飞机
GB2579221A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism
BR112021018640A2 (pt) * 2019-03-21 2021-11-23 AMSL Innovations Pty Ltd Aeronave de decolagem e pouso na vertical (vtol)
CN110866351B (zh) * 2019-09-27 2021-07-27 南京航空航天大学 机翼扰流板增阻微织构设计与基于cfrp材料的制造法
CN110861767A (zh) * 2019-12-13 2020-03-06 贵州贵航飞机设计研究所 一种机翼增升装置组合驱动的方法
CN113104196B (zh) * 2021-05-28 2022-05-24 中国商用飞机有限责任公司 一种用于飞行器的增升装置和增升方法
CN114750930B (zh) * 2022-05-07 2023-05-16 中国航空工业集团公司沈阳飞机设计研究所 一种翼面开缝扰流板式航向控制舵面

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US2272058A (en) * 1938-10-18 1942-02-03 Libbey Owens Ford Glass Co Table top, counter top, or the like
US2261363A (en) 1939-04-29 1941-11-04 United Aireraft Corp Spoiler
US2700516A (en) 1950-01-31 1955-01-25 Phiroze P Nazir Aircraft lift control device
US2772058A (en) * 1951-05-10 1956-11-27 Charles H Grant Aircraft wing with means to increase lift through control of air flow
US2924399A (en) * 1956-04-23 1960-02-09 North American Aviation Inc Aircraft flap structure
US2920844A (en) * 1957-04-12 1960-01-12 North American Aviation Inc Aircraft boundary-layer control system
US2987277A (en) * 1958-10-14 1961-06-06 North American Aviation Inc Aircraft control system
US3131873A (en) * 1963-07-29 1964-05-05 Ryan Aeronautical Co Ejector flap system for aircraft wing with ducted fan
DE1813407C3 (de) 1968-12-07 1974-07-25 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Tragflügel für Luftfahrzeuge mit zumindest einer an der Tragflügelhinterkante befindlichen Hauptklappe
DE1943037C3 (de) 1969-08-23 1978-08-24 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Tragflügel für Luftfahrzeuge, bestehend aus Haupt- und Vorflügel
DE1943680C2 (de) * 1969-08-28 1982-06-24 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Steuerklappenanordnung
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US3757121A (en) * 1972-04-17 1973-09-04 Ulmic Sa Movement of a movable component of an airplane
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US3921942A (en) * 1974-07-01 1975-11-25 Gen Dynamics Corp Rudder boundary layer control device
US4784355A (en) * 1986-11-10 1988-11-15 The United States Of America As Represented By The Secretary Of The Air Force Flap system for short takeoff and landing aircraft
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Also Published As

Publication number Publication date
JP5185105B2 (ja) 2013-04-17
WO2006108579B1 (en) 2007-01-11
RU2399553C2 (ru) 2010-09-20
CN101155726A (zh) 2008-04-02
CN101155726B (zh) 2013-03-13
DE102005016578A1 (de) 2006-10-19
CA2598419A1 (en) 2006-10-19
RU2007141590A (ru) 2009-05-20
US20080179464A1 (en) 2008-07-31
WO2006108579A1 (en) 2006-10-19
US8066228B2 (en) 2011-11-29
JP2008535721A (ja) 2008-09-04
EP1868887A1 (en) 2007-12-26
EP1868887B1 (en) 2011-01-19
CA2598419C (en) 2013-07-23
DE602006019702D1 (de) 2011-03-03

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B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

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B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 10A 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 2384 DE 13-09-2016 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.