BRPI0811030A2 - aeronave - Google Patents

aeronave

Info

Publication number
BRPI0811030A2
BRPI0811030A2 BRPI0811030A BRPI0811030A BRPI0811030A2 BR PI0811030 A2 BRPI0811030 A2 BR PI0811030A2 BR PI0811030 A BRPI0811030 A BR PI0811030A BR PI0811030 A BRPI0811030 A BR PI0811030A BR PI0811030 A2 BRPI0811030 A2 BR PI0811030A2
Authority
BR
Brazil
Prior art keywords
flap
airfoil
rotation axis
aircraft
fuselage
Prior art date
Application number
BRPI0811030A
Other languages
English (en)
Inventor
Cerne Gerd
Original Assignee
Airbus Operations 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 Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0811030A2 publication Critical patent/BRPI0811030A2/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
    • 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
    • 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
BRPI0811030A 2007-04-24 2008-04-24 aeronave BRPI0811030A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US92606707P 2007-04-24 2007-04-24
PCT/EP2008/054985 WO2008129074A1 (en) 2007-04-24 2008-04-24 Aircraft

Publications (1)

Publication Number Publication Date
BRPI0811030A2 true BRPI0811030A2 (pt) 2017-05-09

Family

ID=39684346

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0811030A BRPI0811030A2 (pt) 2007-04-24 2008-04-24 aeronave

Country Status (9)

Country Link
US (1) US8408499B2 (pt)
EP (1) EP2148813B1 (pt)
CN (1) CN101678893B (pt)
AT (1) ATE492468T1 (pt)
BR (1) BRPI0811030A2 (pt)
CA (1) CA2682680C (pt)
DE (1) DE602008004136D1 (pt)
RU (1) RU2009140962A (pt)
WO (1) WO2008129074A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007023394A1 (de) * 2007-05-18 2008-11-20 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators
GB0808349D0 (en) * 2008-05-09 2008-06-18 Airbus Uk Ltd Spoiler deployment mechanism
DE102009002222A1 (de) * 2009-04-06 2010-10-07 Airbus Deutschland Gmbh Flügel eines Flugzeugs oder eines Raumfahrzeugs mit einem beweglichen Strömungskörper
WO2011143794A1 (en) * 2010-05-21 2011-11-24 Airbus S.A.S. Droop panel linkage
DE102010051216A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Seitenrudersystem an einem Flugzeug
DE102011018907A1 (de) * 2011-04-28 2012-10-31 Airbus Operations Gmbh Hochauftriebskomponente für ein Flugzeug, Hochauftriebssystem, Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs und Flugzeug
US8684316B2 (en) 2011-09-23 2014-04-01 The Boeing Company Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions
GB201117340D0 (en) * 2011-10-07 2011-11-23 Airbus Uk Ltd Flat support
CN102642616B (zh) * 2012-05-11 2014-09-17 中国航空工业集团公司西安飞机设计研究所 一种带固定双缝襟翼的飞机增升装置
US10099770B2 (en) * 2013-07-26 2018-10-16 Icon Aircraft, Inc. Manuel wing-fold mechanism
CN103879550A (zh) * 2014-01-16 2014-06-25 李竟儒 一种在飞机机翼下设置有举力装置的飞机
FR3018767B1 (fr) * 2014-03-21 2018-01-12 Airbus Operations Ensemble de support pour un systeme de volet d'aile d'un avion.
CN104400091B (zh) * 2014-12-01 2017-03-08 江西洪都航空工业集团有限责任公司 用于非水平端面的锪工装
CN110072773B (zh) * 2016-12-12 2022-10-21 庞巴迪公司 飞机缝翼
EP3339164A1 (en) * 2016-12-22 2018-06-27 Airbus Operations GmbH Wing for an aircraft
CA3046256A1 (en) * 2018-06-18 2019-12-18 Bombardier Inc. Aircraft wing with deployable flap
US11518496B2 (en) 2019-08-27 2022-12-06 The Boeing Company Flap actuation systems for aircraft
CN112357055B (zh) * 2020-11-23 2022-03-18 西湖大学 一种用于航行器的翼片结构、机翼结构以及航行器

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2246116A (en) * 1937-10-28 1941-06-17 Messerschmitt Boelkow Blohm Airplane wing structure
US2284519A (en) * 1939-09-14 1942-05-26 Bell Aircraft Corp Airplane
GB559546A (en) 1942-05-18 1944-02-24 Phillips & Powis Aircraft Ltd Improvements in aircraft flap actuating gear
US2524605A (en) * 1944-11-23 1950-10-03 Sncaso Arrangement for securing and controlling a movable flap at the trailing edge of an airplane wing
US2670909A (en) * 1950-03-01 1954-03-02 Bell Aircraft Corp Actuating mechanism for aircraft extensible flaps
US4470569A (en) * 1981-12-28 1984-09-11 Mcdonnell Douglas Corporation Locking, redundant slat drive mechanism
US4498647A (en) * 1982-03-15 1985-02-12 Mcdonnel Douglas Corporation Surface hold-down mechanism
US4614320A (en) * 1984-03-27 1986-09-30 Rutan Elbert L Aircraft wing flap
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
US5836550A (en) 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge
US6464176B2 (en) 2000-07-26 2002-10-15 Honda Giken Kogyo Kabushiki Kaisha Flap operating device

Also Published As

Publication number Publication date
ATE492468T1 (de) 2011-01-15
EP2148813B1 (en) 2010-12-22
CN101678893B (zh) 2013-05-22
CA2682680C (en) 2015-11-03
WO2008129074B1 (en) 2008-12-24
CN101678893A (zh) 2010-03-24
CA2682680A1 (en) 2008-10-30
US8408499B2 (en) 2013-04-02
EP2148813A1 (en) 2010-02-03
DE602008004136D1 (de) 2011-02-03
US20100116928A1 (en) 2010-05-13
RU2009140962A (ru) 2011-05-27
WO2008129074A1 (en) 2008-10-30

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]