ATE517030T1 - Tragflügel mit gasabführung - Google Patents

Tragflügel mit gasabführung

Info

Publication number
ATE517030T1
ATE517030T1 AT02769636T AT02769636T ATE517030T1 AT E517030 T1 ATE517030 T1 AT E517030T1 AT 02769636 T AT02769636 T AT 02769636T AT 02769636 T AT02769636 T AT 02769636T AT E517030 T1 ATE517030 T1 AT E517030T1
Authority
AT
Austria
Prior art keywords
aerofoil
wings
gas extraction
trailing
leading
Prior art date
Application number
AT02769636T
Other languages
English (en)
Inventor
Graham Bond Grove
Original Assignee
Graham Bond Grove
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 Graham Bond Grove filed Critical Graham Bond Grove
Application granted granted Critical
Publication of ATE517030T1 publication Critical patent/ATE517030T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/48Varying camber by relatively-movable parts of wing structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/04Boundary layer controls by actively generating fluid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/16Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/28Boundary layer controls at propeller or rotor blades
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/05Variable camber or chord length

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Diaphragms And Bellows (AREA)
AT02769636T 2001-05-11 2002-05-09 Tragflügel mit gasabführung ATE517030T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NZ511661A NZ511661A (en) 2001-05-11 2001-05-11 An improved aerofoil
PCT/NZ2002/000090 WO2002092428A1 (en) 2001-05-11 2002-05-09 Aerofoil with gas discharge

Publications (1)

Publication Number Publication Date
ATE517030T1 true ATE517030T1 (de) 2011-08-15

Family

ID=19928474

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02769636T ATE517030T1 (de) 2001-05-11 2002-05-09 Tragflügel mit gasabführung

Country Status (7)

Country Link
US (1) US7461820B2 (de)
EP (1) EP1392562B1 (de)
AT (1) ATE517030T1 (de)
AU (1) AU2002342476B2 (de)
CA (1) CA2446714C (de)
NZ (1) NZ511661A (de)
WO (1) WO2002092428A1 (de)

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JP4096929B2 (ja) * 2004-08-19 2008-06-04 トヨタ自動車株式会社 垂直離着陸機
EP1674389B1 (de) * 2004-12-22 2007-09-12 Airbus Deutschland GmbH (HRB 43527) Tragwerk einer aerodynamischen Wirkfläche eines Flugzeugs
US7632064B2 (en) * 2006-09-01 2009-12-15 United Technologies Corporation Variable geometry guide vane for a gas turbine engine
RU2531432C2 (ru) * 2012-12-04 2014-10-20 Александр Владимирович Амброжевич Способ создания системы сил летательного аппарата вертикального взлёта и посадки и летательный аппарат для его осуществления
GR20130100618A (el) * 2013-10-25 2015-05-18 Ιωαννης Γεωργιου Μικρος Βελτιωση διεδρων αεροσκαφους στελθ για ταχυτητα
US11325700B2 (en) * 2017-07-21 2022-05-10 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Hypersonic waverider stream surface actuation for variable design point operation
US11518502B2 (en) * 2019-04-30 2022-12-06 Textron Innovations Inc. Energy absorption stabilizers and methods
CN113148222B (zh) * 2021-05-24 2023-01-31 北京航空航天大学 一种适用于复杂前缘形状的密切曲面乘波体正设计方法

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Also Published As

Publication number Publication date
US7461820B2 (en) 2008-12-09
CA2446714C (en) 2009-08-18
EP1392562A4 (de) 2008-03-19
AU2002342476B2 (en) 2008-06-05
US20040253116A1 (en) 2004-12-16
CA2446714A1 (en) 2002-11-21
EP1392562A1 (de) 2004-03-03
EP1392562B1 (de) 2011-07-20
NZ511661A (en) 2003-09-26
WO2002092428A1 (en) 2002-11-21

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties