DE602006007353D1 - Einziebahrer wirbelgenerator - Google Patents
Einziebahrer wirbelgeneratorInfo
- Publication number
- DE602006007353D1 DE602006007353D1 DE602006007353T DE602006007353T DE602006007353D1 DE 602006007353 D1 DE602006007353 D1 DE 602006007353D1 DE 602006007353 T DE602006007353 T DE 602006007353T DE 602006007353 T DE602006007353 T DE 602006007353T DE 602006007353 D1 DE602006007353 D1 DE 602006007353D1
- Authority
- DE
- Germany
- Prior art keywords
- flow control
- vortex generators
- control surface
- flow
- pivot axis
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
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
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Control Of Eletrric Generators (AREA)
- Fluid-Pressure Circuits (AREA)
- Air-Flow Control Members (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69518105P | 2005-06-30 | 2005-06-30 | |
PCT/US2006/025730 WO2007005687A1 (en) | 2005-06-30 | 2006-06-30 | Retractable vortex generator |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602006007353D1 true DE602006007353D1 (de) | 2009-07-30 |
Family
ID=37307191
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602006007353T Active DE602006007353D1 (de) | 2005-06-30 | 2006-06-30 | Einziebahrer wirbelgenerator |
Country Status (12)
Country | Link |
---|---|
US (1) | US7878457B2 (de) |
EP (1) | EP1896323B1 (de) |
JP (1) | JP2008544921A (de) |
KR (1) | KR20080025379A (de) |
CN (1) | CN101213131A (de) |
AT (1) | ATE433909T1 (de) |
AU (1) | AU2006265854A1 (de) |
BR (1) | BRPI0613492A2 (de) |
CA (1) | CA2613446C (de) |
DE (1) | DE602006007353D1 (de) |
RU (1) | RU2008103327A (de) |
WO (1) | WO2007005687A1 (de) |
Families Citing this family (78)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4940434B2 (ja) * | 2005-12-28 | 2012-05-30 | 国立大学法人名古屋大学 | スマートボルテックスジェネレータ及びそれを備えた航空機、船舶、回転機械 |
US7900871B2 (en) * | 2007-07-20 | 2011-03-08 | Textron Innovations, Inc. | Wing leading edge having vortex generators |
FR2920130B1 (fr) * | 2007-08-24 | 2010-01-22 | Airbus France | Dispositif pour generer des perturbations aerodynamiques afin de proteger la surface exterieure d'un aeronef contre des temperatures elevees |
ES2690144T3 (es) * | 2007-11-09 | 2018-11-19 | Bae Systems Plc | Mejoras relacionadas con procedimientos de fabricación de elementos estructurales |
US8047233B2 (en) * | 2007-11-14 | 2011-11-01 | The Boeing Company | Apparatus and method for generating vortexes in fluid flow adjacent to a surface |
US8286909B2 (en) * | 2008-02-08 | 2012-10-16 | Stratocomm Corporation | Boundary layer propulsion airship with related system and method |
US7939178B2 (en) * | 2008-05-14 | 2011-05-10 | Raytheon Company | Shape-changing structure with superelastic foam material |
DE102008033005A1 (de) | 2008-07-14 | 2010-03-18 | Airbus Deutschland Gmbh | Aerodynamische Klappe und Flügel |
US8087617B2 (en) * | 2008-08-15 | 2012-01-03 | The Boeing Company | Retractable nacelle chine |
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 |
US8061986B2 (en) | 2010-06-11 | 2011-11-22 | General Electric Company | Wind turbine blades with controllable aerodynamic vortex elements |
US8038396B2 (en) * | 2010-06-22 | 2011-10-18 | General Electric Company | Vortex generator assembly for use with a wind turbine rotor blade and method for assembling a wind turbine rotor blade |
US8047801B2 (en) | 2010-06-23 | 2011-11-01 | General Electric Company | Wind turbine blades with aerodynamic vortex elements |
US20110142595A1 (en) | 2010-07-02 | 2011-06-16 | General Electric Company | Wind turbine blades with controlled active flow and vortex elements |
US8746053B2 (en) | 2010-12-16 | 2014-06-10 | Inventus Holdings, Llc | Method for determining optimum vortex generator placement for maximum efficiency on a retrofitted wind turbine generator of unknown aerodynamic design |
US8167554B2 (en) | 2011-01-28 | 2012-05-01 | General Electric Corporation | Actuatable surface features for wind turbine rotor blades |
US8852710B2 (en) | 2011-04-08 | 2014-10-07 | Robert B. Evans | Surface flow enhancement device and method of using the same on a vehicle |
US8657238B2 (en) * | 2011-07-05 | 2014-02-25 | The Boeing Company | Retractable vortex generator for reducing stall speed |
EP2548800A1 (de) * | 2011-07-22 | 2013-01-23 | LM Wind Power A/S | Verfahren zum Nachrüsten von Wirbelerzeugern auf einer Windturbinenschaufel |
EP2739528B1 (de) * | 2011-07-22 | 2019-08-28 | LM WP Patent Holding A/S | Wirbelgeneratoranordnung für eine turbinenschaufel |
US9416802B2 (en) | 2012-12-31 | 2016-08-16 | University Of Kansas | Radar energy absorbing deformable low drag vortex generator |
US9464532B2 (en) * | 2013-03-05 | 2016-10-11 | Bell Helicopter Textron Inc. | System and method for reducing rotor blade noise |
US9638176B2 (en) | 2013-05-10 | 2017-05-02 | The Boeing Company | Vortex generator using shape memory alloys |
DE102013210733B4 (de) * | 2013-06-10 | 2021-03-25 | Senvion Gmbh | Rotorblatt und Vortexgenerator |
US9267491B2 (en) | 2013-07-02 | 2016-02-23 | General Electric Company | Wind turbine rotor blade having a spoiler |
US20150211487A1 (en) * | 2014-01-27 | 2015-07-30 | Siemens Aktiengesellschaft | Dual purpose slat-spoiler for wind turbine blade |
US9689374B2 (en) | 2013-10-09 | 2017-06-27 | Siemens Aktiengesellschaft | Method and apparatus for reduction of fatigue and gust loads on wind turbine blades |
US9523279B2 (en) | 2013-11-12 | 2016-12-20 | General Electric Company | Rotor blade fence for a wind turbine |
US9752559B2 (en) | 2014-01-17 | 2017-09-05 | General Electric Company | Rotatable aerodynamic surface features for wind turbine rotor blades |
US9789956B2 (en) | 2014-09-19 | 2017-10-17 | The Boeing Company | Vortex generators responsive to ambient conditions |
US10087912B2 (en) | 2015-01-30 | 2018-10-02 | General Electric Company | Vortex generator for a rotor blade |
DE102015101765A1 (de) * | 2015-02-06 | 2016-08-11 | Airbus Operations Gmbh | Vortexgeneratoranordnung |
DE102015101763A1 (de) | 2015-02-06 | 2016-09-01 | Airbus Operations Gmbh | Seitenleitwerk für ein Flugzeug |
US10252792B2 (en) * | 2015-04-21 | 2019-04-09 | The United States Of America As Represented By The Administrator Of Nasa | Flow disruption devices for the reduction of high lift system noise |
ES2667200T3 (es) * | 2015-10-01 | 2018-05-10 | Airbus Operations Gmbh | Dispositivo generador de turbulencias, sistema de control de flujo y método para controlar un flujo sobre una superficie de timón |
DE102015120958A1 (de) * | 2015-12-02 | 2017-06-08 | Dg Flugzeugbau Gmbh | Aktives Positionieren von Turbulatorflächenelementen |
FR3045012B1 (fr) * | 2015-12-11 | 2017-12-08 | Airbus Operations Sas | Mat d'accrochage d'une turbomachine muni d'un element de protection thermique |
US20170175531A1 (en) * | 2015-12-18 | 2017-06-22 | Amazon Technologies, Inc. | Propeller blade protrusions for improved aerodynamic performance and sound control |
US10011346B2 (en) | 2015-12-18 | 2018-07-03 | Amazon Technologies, Inc. | Propeller blade indentations for improved aerodynamic performance and sound control |
US10259562B2 (en) | 2015-12-18 | 2019-04-16 | Amazon Technologies, Inc. | Propeller blade trailing edge fringes for improved sound control |
US10099773B2 (en) | 2015-12-18 | 2018-10-16 | Amazon Technologies, Inc. | Propeller blade leading edge serrations for improved sound control |
US10232929B2 (en) | 2015-12-18 | 2019-03-19 | Sikorsky Aircraft Corporation | Plate member for reducing drag on a fairing of an aircraft |
US10220939B2 (en) | 2015-12-18 | 2019-03-05 | Sikorsky Aircraft Corporation | Active airflow system and method of reducing drag for aircraft |
US10460717B2 (en) | 2015-12-18 | 2019-10-29 | Amazon Technologies, Inc. | Carbon nanotube transducers on propeller blades for sound control |
US10933988B2 (en) | 2015-12-18 | 2021-03-02 | Amazon Technologies, Inc. | Propeller blade treatments for sound control |
US10259574B2 (en) | 2015-12-18 | 2019-04-16 | Amazon Technologies, Inc. | Propeller surface area treatments for sound dampening |
US20170174326A1 (en) * | 2015-12-18 | 2017-06-22 | Sikorsky Aircraft Corporation | Vortex generators and method of creating vortices on an aircraft |
JP6719933B2 (ja) * | 2016-03-16 | 2020-07-08 | 三菱重工業株式会社 | ジェットエンジン、飛しょう体、および、ジェットエンジンの動作方法 |
EP3267031B1 (de) | 2016-07-05 | 2019-06-12 | Siemens Gamesa Renewable Energy A/S | Windturbinenrotorblatt mit wirbelerzeugern |
US10487796B2 (en) | 2016-10-13 | 2019-11-26 | General Electric Company | Attachment methods for surface features of wind turbine rotor blades |
EP3323716B1 (de) * | 2016-11-21 | 2020-01-01 | Airbus Operations GmbH | Flugzeugluftstrommodifizierungsvorrichtung und wirbelgeneratoranordnung für ein flugzeug |
US9939391B1 (en) | 2016-12-15 | 2018-04-10 | Bell Helicopter Textron Inc. | Inspection method using a film overlay |
US10352906B2 (en) | 2016-12-15 | 2019-07-16 | Bell Helicopter Textron Inc. | Through-transmission ultrasonic testing apparatus |
US10994826B2 (en) * | 2017-01-12 | 2021-05-04 | The Boeing Company | Temperature sensitive self actuated heat boundary layer control device |
US10465652B2 (en) | 2017-01-26 | 2019-11-05 | General Electric Company | Vortex generators for wind turbine rotor blades having noise-reducing features |
US10889370B2 (en) * | 2018-07-02 | 2021-01-12 | Textron Innovations Inc. | Chord-wise variable vortex generator |
CN108910019B (zh) * | 2018-07-05 | 2020-03-31 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种采用热双金属微锯齿结构的空气流动控制系统 |
US11163302B2 (en) | 2018-09-06 | 2021-11-02 | Amazon Technologies, Inc. | Aerial vehicle propellers having variable force-torque ratios |
DE102018127804B4 (de) | 2018-11-07 | 2024-07-25 | Vc Viii Polytech Holding Aps | Verbesserung bzw. Optimierung des Ertrags einer Windenergieanlage durch Detektion eines Strömungsabrisses |
US11066149B2 (en) * | 2018-11-21 | 2021-07-20 | The Boeing Company | Airflow-dependent deployable fences for aircraft wings |
US11059564B2 (en) * | 2018-11-21 | 2021-07-13 | The Boeing Company | Automated deployable fences for aircraft wings |
US11059565B2 (en) | 2018-11-21 | 2021-07-13 | The Boeing Company | Airflow-dependent deployable fences for aircraft wings |
US11130561B2 (en) * | 2018-11-21 | 2021-09-28 | The Boeing Company | Airflow-dependent deployable fences for aircraft wings |
CN110435876B (zh) * | 2019-08-26 | 2020-06-19 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种带有伸缩式涡流发生器的共轴旋翼桨毂整流罩 |
US11407498B2 (en) | 2019-08-30 | 2022-08-09 | The Boeing Company | Vortex generator passive deployment system |
US12065236B2 (en) * | 2020-01-23 | 2024-08-20 | Enterprise Science Fund, Llc | Systems and methods for active control of surface drag using intermittent or variable actuation |
US11905983B2 (en) | 2020-01-23 | 2024-02-20 | Deep Science, Llc | Systems and methods for active control of surface drag using electrodes |
US11643190B2 (en) * | 2020-01-30 | 2023-05-09 | Airbus Operations Gmbh | Vortex generator apparatus for an aircraft |
AU2021313417A1 (en) | 2020-07-23 | 2023-02-09 | Bae Systems Plc | Arrangements, duct arrangements and methods |
GB2597660B (en) * | 2020-07-23 | 2024-08-21 | Bae Systems Plc | Duct arrangements and methods |
GB2597659A (en) * | 2020-07-23 | 2022-02-09 | Bae Systems Plc | Arrangements, duct arrangements and methods |
GB2597661B (en) * | 2020-07-23 | 2024-05-22 | Bae Systems Plc | Arrangements, duct arrangements and methods |
EP4185526A1 (de) | 2020-07-23 | 2023-05-31 | BAE SYSTEMS plc | Anordnung zur beeinflussung eines flüssigkeitsstroms und verfahren |
EP4032810A1 (de) | 2021-01-22 | 2022-07-27 | Blue Spirit Aero SAS | Flugzeug mit elektrischem antriebsmodul |
US20240076035A1 (en) * | 2021-01-22 | 2024-03-07 | Blue Spirit Aero Sas | Aircraft having retractable vortex generators |
US11466709B2 (en) | 2021-02-17 | 2022-10-11 | Deep Science, Llc | In-plane transverse momentum injection to disrupt large-scale eddies in a turbulent boundary layer |
CN114954920B (zh) * | 2022-03-14 | 2024-06-28 | 南京航空航天大学 | 气流流动方向可变的电弧放电激励器装置及工作方法 |
JP7568145B2 (ja) | 2022-03-30 | 2024-10-16 | 大日本印刷株式会社 | 構造体及び構造体を備える物体 |
Family Cites Families (32)
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US1763257A (en) * | 1928-04-25 | 1930-06-10 | David L Roscoe | Aerofoil |
US2764373A (en) * | 1953-05-18 | 1956-09-25 | Boeing Co | Heated vortex generator |
US2959377A (en) * | 1957-03-15 | 1960-11-08 | Poly Ind Inc | Airfoil structure with boundary layer control means |
US3090580A (en) * | 1962-04-13 | 1963-05-21 | Alan B Kehlet | Space and atmospheric re-entry vehicle |
US4039161A (en) * | 1975-10-16 | 1977-08-02 | Mcdonnell Douglas Corporation | Hidden vortex generators |
US4017041A (en) * | 1976-01-12 | 1977-04-12 | Nelson Wilbur C | Airfoil tip vortex control |
US4466586A (en) | 1980-03-10 | 1984-08-21 | The Boeing Company | Directional control device for aircraft |
SE8101793L (sv) * | 1980-03-25 | 1981-09-26 | Nat Res Dev | Luftplan |
SE450480B (sv) * | 1982-08-30 | 1987-06-29 | Tech Gerete Und Entwicklungsge | Styvvingad flygkropp |
US4932610A (en) * | 1986-03-11 | 1990-06-12 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Active control of boundary layer transition and turbulence |
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US5062595A (en) * | 1990-04-26 | 1991-11-05 | University Of Southern California | Delta wing with lift enhancing flap |
US5253828A (en) * | 1992-07-17 | 1993-10-19 | The Board Of Regents Of The University Of Oklahoma | Concealable flap-actuated vortex generator |
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 |
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US5785282A (en) * | 1995-08-18 | 1998-07-28 | Sikorsky Aircraft Corporation | Half-plow vortex generators for rotorcraft blades for reducing blade-vortex interaction noise |
US5788191A (en) * | 1995-08-18 | 1998-08-04 | Sikorsky Aircraft Corporation | Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise |
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US6168111B1 (en) * | 1997-03-03 | 2001-01-02 | The United States Of America As Represented By The Secretary Of The Army | Fold-out fin |
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US6161800A (en) * | 1999-05-04 | 2000-12-19 | The Boeing Company | Pivoting spanwise-flow redirector for tiltrotor aircraft |
WO2001087706A1 (en) * | 2000-05-16 | 2001-11-22 | Bell Helicopter Textron Inc. | Multi-mode tiltrotor nacelle control system with integrated envelope protection |
US6427948B1 (en) * | 2000-10-30 | 2002-08-06 | Michael Campbell | Controllable vortex generator |
US6478541B1 (en) * | 2001-08-16 | 2002-11-12 | The Boeing Company | Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction |
US6837465B2 (en) * | 2003-01-03 | 2005-01-04 | Orbital Research Inc | Flow control device and method of controlling flow |
US6892982B2 (en) * | 2003-01-29 | 2005-05-17 | Northrop Grumman Corporation | Aircraft with forward opening inlay spoilers for yaw control |
-
2006
- 2006-06-30 AU AU2006265854A patent/AU2006265854A1/en not_active Abandoned
- 2006-06-30 CN CNA2006800237307A patent/CN101213131A/zh active Pending
- 2006-06-30 EP EP06786059A patent/EP1896323B1/de active Active
- 2006-06-30 DE DE602006007353T patent/DE602006007353D1/de active Active
- 2006-06-30 WO PCT/US2006/025730 patent/WO2007005687A1/en active Application Filing
- 2006-06-30 AT AT06786059T patent/ATE433909T1/de not_active IP Right Cessation
- 2006-06-30 US US11/477,806 patent/US7878457B2/en active Active
- 2006-06-30 KR KR1020077030518A patent/KR20080025379A/ko not_active Application Discontinuation
- 2006-06-30 BR BRPI0613492-0A patent/BRPI0613492A2/pt not_active Application Discontinuation
- 2006-06-30 JP JP2008519640A patent/JP2008544921A/ja active Pending
- 2006-06-30 CA CA2613446A patent/CA2613446C/en active Active
- 2006-06-30 RU RU2008103327/11A patent/RU2008103327A/ru not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US7878457B2 (en) | 2011-02-01 |
CA2613446A1 (en) | 2007-01-11 |
ATE433909T1 (de) | 2009-07-15 |
EP1896323B1 (de) | 2009-06-17 |
KR20080025379A (ko) | 2008-03-20 |
JP2008544921A (ja) | 2008-12-11 |
RU2008103327A (ru) | 2009-08-10 |
CA2613446C (en) | 2016-11-22 |
EP1896323A1 (de) | 2008-03-12 |
BRPI0613492A2 (pt) | 2011-01-11 |
AU2006265854A1 (en) | 2007-01-11 |
US20070018056A1 (en) | 2007-01-25 |
CN101213131A (zh) | 2008-07-02 |
WO2007005687A1 (en) | 2007-01-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |