ATE465944T1 - Systeme und verfahren zur destabilisierung eines schaufelwirbels - Google Patents
Systeme und verfahren zur destabilisierung eines schaufelwirbelsInfo
- 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
Links
- 230000000368 destabilizing effect Effects 0.000 title 1
- 239000012530 fluid Substances 0.000 abstract 6
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
- B64C23/069—Influencing 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
- B64C23/076—Influencing 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
-
- 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
- Y02T50/10—Drag 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)
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)
| 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 |
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| 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 |
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| JPH08133188A (ja) * | 1994-11-07 | 1996-05-28 | Mitsubishi Heavy Ind Ltd | 翼の抵抗低減装置 |
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| US5845874A (en) | 1996-10-29 | 1998-12-08 | Silicon Graphics, Inc. | System and method for creating visual images of aircraft wake vortices |
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| US6425553B1 (en) | 1999-08-20 | 2002-07-30 | West Virginia University | Piezoelectric actuators for circulation controlled rotorcraft |
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| 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 |
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| 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 |
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| 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 |
-
2006
- 2006-03-07 US US11/370,099 patent/US7661629B2/en not_active Expired - Lifetime
-
2007
- 2007-03-02 JP JP2008558306A patent/JP5205284B2/ja active Active
- 2007-03-02 EP EP07861254A patent/EP1999014B1/de active Active
- 2007-03-02 DE DE602007006170T patent/DE602007006170D1/de active Active
- 2007-03-02 WO PCT/US2007/005253 patent/WO2008051269A2/en not_active Ceased
- 2007-03-02 AT AT07861254T patent/ATE465944T1/de not_active IP Right Cessation
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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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |