ATE465944T1 - Systeme und verfahren zur destabilisierung eines schaufelwirbels - Google Patents

Systeme und verfahren zur destabilisierung eines schaufelwirbels

Info

Publication number
ATE465944T1
ATE465944T1 AT07861254T AT07861254T ATE465944T1 AT E465944 T1 ATE465944 T1 AT E465944T1 AT 07861254 T AT07861254 T AT 07861254T AT 07861254 T AT07861254 T AT 07861254T AT E465944 T1 ATE465944 T1 AT E465944T1
Authority
AT
Austria
Prior art keywords
fluid
valve device
methods
tip
flow
Prior art date
Application number
AT07861254T
Other languages
English (en)
Inventor
Arvin Shmilovich
Yoram Yadlin
Roger W Clark
Donald H Leopold
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE465944T1 publication Critical patent/ATE465944T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069Influencing 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
    • B64C23/076Influencing 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Processing Of Solid Wastes (AREA)
AT07861254T 2006-03-07 2007-03-02 Systeme und verfahren zur destabilisierung eines schaufelwirbels ATE465944T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/370,099 US7661629B2 (en) 2004-02-20 2006-03-07 Systems and methods for destabilizing an airfoil vortex
PCT/US2007/005253 WO2008051269A2 (en) 2006-03-07 2007-03-02 Systems and methods for destabilizing an airfoil vortex

Publications (1)

Publication Number Publication Date
ATE465944T1 true ATE465944T1 (de) 2010-05-15

Family

ID=39325068

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07861254T ATE465944T1 (de) 2006-03-07 2007-03-02 Systeme und verfahren zur destabilisierung eines schaufelwirbels

Country Status (6)

Country Link
US (1) US7661629B2 (de)
EP (1) EP1999014B1 (de)
JP (1) JP5205284B2 (de)
AT (1) ATE465944T1 (de)
DE (1) DE602007006170D1 (de)
WO (1) WO2008051269A2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8016244B2 (en) * 2004-02-20 2011-09-13 The Boeing Company Active systems and methods for controlling an airfoil vortex
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
US7686253B2 (en) * 2006-08-10 2010-03-30 The Boeing Company Systems and methods for tracing aircraft vortices
KR101112145B1 (ko) 2007-02-09 2012-02-22 삼성전자주식회사 이동통신 시스템의 랜덤 액세스 프로시져에서 경쟁의 감지 방법 및 장치
GB0802000D0 (en) * 2008-02-04 2008-03-12 Wingtec Holdings Ltd Aerofoil control devices
JP5286527B2 (ja) * 2009-07-13 2013-09-11 三菱重工業株式会社 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
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
US8413501B2 (en) * 2010-03-26 2013-04-09 The Boeing Company Wake measurement probe
GB2468978B (en) * 2010-04-27 2012-04-04 Aerodynamic Res Innovation Holdings Ltd Fluid flow control device for an aerofoil
GB201011843D0 (en) * 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
GB201103122D0 (en) * 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
US20170088254A1 (en) * 2011-03-10 2017-03-30 RuiQing Hong Ultra-High-Pressure Fluid Injection Dynamic Orbit-Transfer System and Method
CN102167162A (zh) * 2011-03-10 2011-08-31 洪瑞庆 一种用于飞行器的超高压流体喷射动力变轨系统及方法
US9227719B2 (en) * 2011-03-11 2016-01-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reactive orthotropic lattice diffuser for noise reduction
US9132909B1 (en) * 2011-03-11 2015-09-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flap edge noise reduction fins
US8632031B2 (en) * 2011-04-11 2014-01-21 The Boeing Company Systems and methods for attenuation of noise and wakes produced by aircraft
RU2469411C1 (ru) * 2011-06-02 2012-12-10 Федеральное государственное унитарное предприятие "Государственный научно-исследовательский институт авиационных систем" Способ информационного обеспечения вихревой безопасности полета летательных аппаратов
RU2477893C1 (ru) * 2011-09-30 2013-03-20 Федеральное государственное унитарное предприятие "Государственный научно-исследовательский институт авиационных систем" Способ обеспечения вихревой безопасности полета летательного аппарата
US9896192B2 (en) 2011-12-13 2018-02-20 Lockheed Martin Corroration Minimally intrusive wingtip vortex wake mitigation using microvane arrays
CA2957428A1 (en) 2014-08-05 2016-02-11 The Procter & Gamble Company Fibrous structures
US10132042B2 (en) 2015-03-10 2018-11-20 The Procter & Gamble Company Fibrous structures
GB2535488A (en) * 2015-02-17 2016-08-24 Airbus Operations Ltd An arrangement for effecting movement of a wing tip device between a flight configuration and a ground configuration
DE102015107626B4 (de) * 2015-05-15 2019-11-07 Airbus Defence and Space GmbH Strömungssteuerungsvorrichtung, Strömungsdynamischer Profilkörper und Strömungssteuerungsverfahren mit Schallwellenerzeugung
US11408129B2 (en) 2018-12-10 2022-08-09 The Procter & Gamble Company Fibrous structures
US12265766B2 (en) 2020-08-03 2025-04-01 The Boeing Company Methods and apparatus to improve fluid flow simulations
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

Family Cites Families (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2477461A (en) 1943-07-29 1949-07-26 United Aircraft Corp Rotating jet device for airfoils
US2650781A (en) 1950-08-11 1953-09-01 United Aircraft Corp Boundary layer control for aircraft
US3090584A (en) * 1956-08-15 1963-05-21 Power Jets Res & Dev Ltd Aircraft
US3012740A (en) 1958-04-04 1961-12-12 Fairchild Stratos Corp Aircraft boundary layer control system
US3480234A (en) 1967-08-18 1969-11-25 Lockheed Aircraft Corp Method and apparatus for modifying airfoil fluid flow
DE1756541C3 (de) 1968-06-04 1974-10-24 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flugzeug mit einer Ausblaseeinrichtung
US3596854A (en) 1969-06-09 1971-08-03 William R Haney Jr Vortex generator for airfoil structures
US3604661A (en) 1969-09-25 1971-09-14 Robert Alfred Mayer Jr Boundary layer control means
US3692259A (en) 1970-06-26 1972-09-19 Shao Wen Yuan Wing-tip vortices control
US3761929A (en) 1971-02-24 1973-09-25 Us Navy Radar spoof
US3845918A (en) 1972-12-07 1974-11-05 Rochester Applied Science Ass Vortex dissipator
US3841587A (en) 1973-03-16 1974-10-15 L Freed Vortex arrestor and visualization system
US3881669A (en) 1973-05-16 1975-05-06 Martin Lessen Method and apparatus for elimination of airfoil trailing vortices
US3974986A (en) 1973-05-29 1976-08-17 Johnstone Edmund H Aircraft wing vortex deflector
US3936013A (en) 1973-12-17 1976-02-03 Shao Wen Yuan Vortex control
US3984070A (en) 1974-05-24 1976-10-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Wingtip vortex dissipator for aircraft
US3997132A (en) 1974-12-11 1976-12-14 The Garrett Corporation Method and apparatus for controlling tip vortices
JPS52121297A (en) * 1976-04-03 1977-10-12 Masaaki Kusano High lift apparatus
US4477042A (en) 1981-01-19 1984-10-16 Griswold Ii Roger W Vortex alleviating wing tip
US5150859A (en) 1986-12-22 1992-09-29 Sundstrand Corporation Wingtip turbine
US4860976A (en) 1987-10-05 1989-08-29 The Boeing Company Attached jet spanwise blowing lift augmentation system
JPH04108095A (ja) * 1990-08-28 1992-04-09 Mitsubishi Heavy Ind Ltd 航空機
US5158251A (en) 1990-11-16 1992-10-27 The United State Of America As Represented By The Secretary Of The Navy Aerodynamic surface tip vortex attenuation system
WO1993022196A1 (en) 1992-04-28 1993-11-11 British Technology Group Usa Inc. Lifting body with reduced-strength trailing vortices
JP2951540B2 (ja) 1994-06-30 1999-09-20 川田工業株式会社 回転翼航空機の低騒音化装置
US5634613A (en) 1994-07-18 1997-06-03 Mccarthy; Peter T. Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect
JPH08133188A (ja) * 1994-11-07 1996-05-28 Mitsubishi Heavy Ind Ltd 翼の抵抗低減装置
US5755408A (en) 1995-04-03 1998-05-26 Schmidt; Robert N. Fluid flow control devices
US5758823A (en) 1995-06-12 1998-06-02 Georgia Tech Research Corporation Synthetic jet actuator and applications thereof
US6123145A (en) 1995-06-12 2000-09-26 Georgia Tech Research Corporation Synthetic jet actuators for cooling heated bodies and environments
US5806807A (en) 1995-10-04 1998-09-15 Haney; William R. Airfoil vortex attenuation apparatus and method
US5813625A (en) 1996-10-09 1998-09-29 Mcdonnell Douglas Helicopter Company Active blowing system for rotorcraft vortex interaction noise reduction
US5845874A (en) 1996-10-29 1998-12-08 Silicon Graphics, Inc. System and method for creating visual images of aircraft wake vortices
US5938404A (en) 1997-06-05 1999-08-17 Mcdonnell Douglas Helicopter Company Oscillating air jets on aerodynamic surfaces
US6082679A (en) 1997-06-26 2000-07-04 The Boeing Company Active system for early destruction of trailing vortices
US5918835A (en) 1998-03-11 1999-07-06 Northrop Grumman Corporation Wingtip vortex impeller device for reducing drag and vortex cancellation
US6129309A (en) 1998-07-24 2000-10-10 Mcdonnell Douglas Corporation Aircraft engine apparatus with reduced inlet vortex
US6138955A (en) 1998-12-23 2000-10-31 Board Of Supervisors Of Louisiana State University And Agricultural And Mechanical College Vortical lift control over a highly swept wing
US6425553B1 (en) 1999-08-20 2002-07-30 West Virginia University Piezoelectric actuators for circulation controlled rotorcraft
US6554607B1 (en) 1999-09-01 2003-04-29 Georgia Tech Research Corporation Combustion-driven jet actuator
US6283406B1 (en) 1999-09-10 2001-09-04 Gte Service Corporation Use of flow injection and extraction to control blade vortex interaction and high speed impulsive noise in helicopters
DE19950403C2 (de) 1999-10-20 2002-02-07 Deutsch Zentr Luft & Raumfahrt Flugzeug mit Mitteln zum Reduzieren der Wirbelstärke des Flügelhauptwirbelpaars
JP2001247095A (ja) 2000-03-03 2001-09-11 Okinaga Tomioka 除雪装置付き航空機
DE10018389C2 (de) 2000-04-13 2003-12-18 Airbus Gmbh Vorrichtung sowie Verfahren zur Reduzierung von Nachlaufwirbeln hinter Flugzeugen im Landeanflug
DE10039109A1 (de) 2000-08-07 2002-02-28 Gunther Schaenzer Verfahren und Einrichtung zur Bestimmung des störenden Einflusses einer Wirbelschleppe
JP3570360B2 (ja) 2000-08-31 2004-09-29 三菱電機株式会社 後方乱気流検出システム
US6394397B1 (en) 2000-12-06 2002-05-28 The Boeing Company Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith
US6471477B2 (en) 2000-12-22 2002-10-29 The Boeing Company Jet actuators for aerodynamic surfaces
US6668638B2 (en) 2001-05-25 2003-12-30 National Research Council Of Canada Active vortex control with moveable jet
US6963291B2 (en) 2002-05-17 2005-11-08 The Board Of Trustees Of The Leland Stanford Junior University Dynamic wake prediction and visualization with uncertainty analysis
US6629674B1 (en) 2002-07-24 2003-10-07 General Electric Company Method and apparatus for modulating airfoil lift
US7017862B1 (en) 2003-01-08 2006-03-28 Fischbach Jack T Wake vortex visualizer for an aircraft
US7333030B2 (en) 2003-07-25 2008-02-19 Joint Stock Company “Spetstekhnika” Method and system for preventing an aircraft from penetrating into a dangerous trailing vortex area of a vortex generator
US7300693B2 (en) 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US8016244B2 (en) 2004-02-20 2011-09-13 The Boeing Company Active systems and methods for controlling an airfoil vortex
US7100875B2 (en) * 2004-02-20 2006-09-05 The Boeing Company Apparatus and method for the control of trailing wake flows
US7510149B2 (en) * 2004-08-02 2009-03-31 Lockheed Martin Corporation System and method to control flowfield vortices with micro-jet arrays
US7635107B2 (en) 2005-08-09 2009-12-22 The Boeing Company System for aerodynamic flows and associated method
US8033510B2 (en) 2005-08-09 2011-10-11 The Boeing Company Lift augmentation system and associated method
US7104143B1 (en) 2005-08-11 2006-09-12 The Boeing Company Oscillating vane actuator apparatus and method for active flow control
US20080035784A1 (en) 2006-08-10 2008-02-14 Meserole Jere S Aircraft wake vortex predictor and visualizer
US7686253B2 (en) 2006-08-10 2010-03-30 The Boeing Company Systems and methods for tracing aircraft vortices
GB2468978B (en) * 2010-04-27 2012-04-04 Aerodynamic Res Innovation Holdings Ltd Fluid flow control device for an aerofoil

Also Published As

Publication number Publication date
JP2009533259A (ja) 2009-09-17
DE602007006170D1 (de) 2010-06-10
JP5205284B2 (ja) 2013-06-05
WO2008051269A2 (en) 2008-05-02
US7661629B2 (en) 2010-02-16
EP1999014A2 (de) 2008-12-10
US20090173835A1 (en) 2009-07-09
WO2008051269A3 (en) 2008-07-24
WO2008051269B1 (en) 2008-09-12
EP1999014B1 (de) 2010-04-28

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