BR112012001678A2 - dispositivo de alta sustentação, asa e dispositivo de redução de ruído para o dispositivo de alta sutentação - Google Patents

dispositivo de alta sustentação, asa e dispositivo de redução de ruído para o dispositivo de alta sutentação

Info

Publication number
BR112012001678A2
BR112012001678A2 BR112012001678A BR112012001678A BR112012001678A2 BR 112012001678 A2 BR112012001678 A2 BR 112012001678A2 BR 112012001678 A BR112012001678 A BR 112012001678A BR 112012001678 A BR112012001678 A BR 112012001678A BR 112012001678 A2 BR112012001678 A2 BR 112012001678A2
Authority
BR
Brazil
Prior art keywords
wing
noise reduction
suture
support device
high support
Prior art date
Application number
BR112012001678A
Other languages
English (en)
Other versions
BR112012001678B1 (pt
Inventor
Kazuomi Yamamoto
Keizo Takenaka
Makoto Hirai
Taro Imamura
Yuzuru Yokokawa
Original Assignee
Japan Aerospace Exploration
Mitsubishi Heavy Ind Ltd
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 Japan Aerospace Exploration, Mitsubishi Heavy Ind Ltd filed Critical Japan Aerospace Exploration
Publication of BR112012001678A2 publication Critical patent/BR112012001678A2/pt
Publication of BR112012001678B1 publication Critical patent/BR112012001678B1/pt

Links

Classifications

    • 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
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Wind Motors (AREA)
  • Braking Arrangements (AREA)
BR112012001678-4A 2009-07-13 2010-07-12 Dispositivo de alta sustentação, asa e dispositivo de redução de ruído BR112012001678B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2009164869A JP5286527B2 (ja) 2009-07-13 2009-07-13 高揚力発生装置、翼および高揚力発生装置の騒音低減装置
JP2009-164869 2009-07-13
PCT/JP2010/061777 WO2011007759A1 (ja) 2009-07-13 2010-07-12 高揚力発生装置、翼および高揚力発生装置の騒音低減装置

Publications (2)

Publication Number Publication Date
BR112012001678A2 true BR112012001678A2 (pt) 2016-04-12
BR112012001678B1 BR112012001678B1 (pt) 2020-09-29

Family

ID=43449367

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012001678-4A BR112012001678B1 (pt) 2009-07-13 2010-07-12 Dispositivo de alta sustentação, asa e dispositivo de redução de ruído

Country Status (8)

Country Link
US (1) US9440729B2 (pt)
EP (1) EP2455282B1 (pt)
JP (1) JP5286527B2 (pt)
CN (1) CN102470918B (pt)
BR (1) BR112012001678B1 (pt)
CA (1) CA2767990C (pt)
RU (1) RU2517540C2 (pt)
WO (1) WO2011007759A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170088254A1 (en) * 2011-03-10 2017-03-30 RuiQing Hong Ultra-High-Pressure Fluid Injection Dynamic Orbit-Transfer System and Method
JP6569303B2 (ja) * 2015-05-28 2019-09-04 三菱航空機株式会社 フラップおよび航空機
JP6486201B2 (ja) * 2015-05-28 2019-03-20 国立研究開発法人宇宙航空研究開発機構 翼、フラップおよび航空機
DE102018121395B4 (de) * 2018-09-03 2021-06-17 Airbus Defence and Space GmbH Endrippenanordnung für eine Auftriebshilfevorrichtung eines Luftfahrzeugs mit Lärmminderung
CN112810803A (zh) * 2021-02-22 2021-05-18 中国民用航空飞行学院 一种用于加快翼尖涡耗散的飞机尾流调整装置
CN116735142B (zh) * 2023-08-14 2023-10-20 中国航空工业集团公司沈阳空气动力研究所 一种连续式跨声速风洞透气壁试验段背景噪声抑制方法

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US880417A (en) * 1905-03-09 1908-02-25 William Joseph Still Apparatus for transmitting heat from one fluid to another.
US1994045A (en) * 1932-06-16 1935-03-12 Nelson Henry Wade Airplane
US2119089A (en) * 1933-07-21 1938-05-31 Zap Dev Corp Flap construction
US2207453A (en) * 1937-10-02 1940-07-09 Arado Flugzeugwerke Gmbh Aircraft supporting wing
GB880417A (en) * 1957-05-13 1961-10-18 Jacques Jean Marie Jules Gerin Extensible device for aircraft wings
US3199813A (en) * 1964-06-03 1965-08-10 Boeing Co Aircraft airfoil pods
US3596854A (en) * 1969-06-09 1971-08-03 William R Haney Jr Vortex generator for airfoil structures
US5738298A (en) * 1995-06-08 1998-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tip fence for reduction of lift-generated airframe noise
US5806807A (en) * 1995-10-04 1998-09-15 Haney; William R. Airfoil vortex attenuation apparatus and method
RU2174483C2 (ru) * 1998-07-13 2001-10-10 Центральный аэрогидродинамический институт им. проф. Н.Е. Жуковского Устройство для ослабления вихревого следа механизированного крыла (варианты)
DE10018389C2 (de) * 2000-04-13 2003-12-18 Airbus Gmbh Vorrichtung sowie Verfahren zur Reduzierung von Nachlaufwirbeln hinter Flugzeugen im Landeanflug
DE10020177A1 (de) * 2000-04-25 2001-11-08 Daimler Chrysler Ag Einrichtung zur Lärmminderung an Tragflügeln von Flugzeugen
WO2004002823A1 (en) * 2002-06-26 2004-01-08 Mccarthy Peter T High efficiency tip vortex reversal and induced drag reduction
US7661629B2 (en) * 2004-02-20 2010-02-16 The Boeing Company Systems and methods for destabilizing an airfoil vortex
DE102004056537B4 (de) * 2004-11-23 2010-09-09 Eads Deutschland Gmbh Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
DE102006008434A1 (de) * 2006-02-23 2007-09-06 Airbus Deutschland Gmbh Vorrichtung zur Reduzierung des aerodynamisch bedingten Lärms an der Seitenkante einer Stellfläche, insbesondere einer Hochauftriebsfläche eines Flugzeugs
US7874524B2 (en) * 2007-11-16 2011-01-25 The Boeing Company Methods and apparatus for a multi-segment flap fence
US20110006165A1 (en) * 2009-07-10 2011-01-13 Peter Ireland Application of conformal sub boundary layer vortex generators to a foil or aero/ hydrodynamic surface
US8708272B1 (en) * 2011-03-11 2014-04-29 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Landing gear door liners for airframe noise reduction

Also Published As

Publication number Publication date
JP2011020476A (ja) 2011-02-03
US9440729B2 (en) 2016-09-13
US20120145826A1 (en) 2012-06-14
JP5286527B2 (ja) 2013-09-11
EP2455282A4 (en) 2012-11-21
RU2012100039A (ru) 2013-08-20
CA2767990C (en) 2014-05-27
CN102470918B (zh) 2015-03-25
RU2517540C2 (ru) 2014-05-27
EP2455282A1 (en) 2012-05-23
WO2011007759A1 (ja) 2011-01-20
BR112012001678B1 (pt) 2020-09-29
EP2455282B1 (en) 2014-10-15
CN102470918A (zh) 2012-05-23
CA2767990A1 (en) 2011-01-20

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according art. 34 industrial property law
B06U Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure
B06A Notification to applicant to reply to the report for non-patentability or inadequacy of the application according art. 36 industrial patent law
B09A Decision: intention to grant
B16A Patent or certificate of addition of invention granted

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