ES2387001T5 - Aparato y método para controlar el flujo de plasma en el borde de salida de un perfil aerodinámico - Google Patents
Aparato y método para controlar el flujo de plasma en el borde de salida de un perfil aerodinámicoInfo
- Publication number
- ES2387001T5 ES2387001T5 ES08156375T ES08156375T ES2387001T5 ES 2387001 T5 ES2387001 T5 ES 2387001T5 ES 08156375 T ES08156375 T ES 08156375T ES 08156375 T ES08156375 T ES 08156375T ES 2387001 T5 ES2387001 T5 ES 2387001T5
- Authority
- ES
- Spain
- Prior art keywords
- trailing edge
- coanda surface
- plasma flow
- aerodynamic profile
- controlling plasma
- 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
- 238000000034 method Methods 0.000 title abstract 3
- 238000000926 separation method Methods 0.000 abstract 3
- 230000009977 dual effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/2406—Generating plasma using dielectric barrier discharges, i.e. with a dielectric interposed between the electrodes
- H05H1/2439—Surface discharges, e.g. air flow control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
-
- 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)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Plasma Technology (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/753,857 US7988101B2 (en) | 2007-05-25 | 2007-05-25 | Airfoil trailing edge plasma flow control apparatus and method |
| US753857 | 2007-05-25 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES2387001T3 ES2387001T3 (es) | 2012-09-11 |
| ES2387001T5 true ES2387001T5 (es) | 2016-05-27 |
Family
ID=39561803
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES08156375T Active ES2387001T5 (es) | 2007-05-25 | 2008-05-16 | Aparato y método para controlar el flujo de plasma en el borde de salida de un perfil aerodinámico |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US7988101B2 (es) |
| EP (1) | EP1995171B2 (es) |
| JP (1) | JP5354955B2 (es) |
| CN (1) | CN101332871B (es) |
| AT (1) | ATE555985T1 (es) |
| ES (1) | ES2387001T5 (es) |
| RU (1) | RU2474513C2 (es) |
Families Citing this family (66)
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| US8348626B2 (en) * | 2007-07-25 | 2013-01-08 | University Of Florida Research Foundation, Inc. | Method and apparatus for efficient micropumping |
| US9200522B2 (en) * | 2007-12-14 | 2015-12-01 | University Of Florida Research Foundation, Inc. | Active film cooling for turbine blades |
| US8220753B2 (en) | 2008-01-04 | 2012-07-17 | The Boeing Company | Systems and methods for controlling flows with pulsed discharges |
| US9446840B2 (en) * | 2008-07-01 | 2016-09-20 | The Boeing Company | Systems and methods for alleviating aircraft loads with plasma actuators |
| US8251318B2 (en) * | 2008-11-19 | 2012-08-28 | The Boeing Company | Disbanded cascaded array for generating and moving plasma clusters for active airflow control |
| CN101784155B (zh) * | 2009-01-21 | 2012-05-02 | 郝江南 | 一种等离子体双极性激励电极 |
| US8157528B1 (en) | 2009-04-29 | 2012-04-17 | The Boeing Company | Active directional control of airflows over rotorcraft blades using plasma actuating cascade arrays |
| US8162610B1 (en) | 2009-05-26 | 2012-04-24 | The Boeing Company | Active directional control of airflows over wind turbine blades using plasma actuating cascade arrays |
| WO2011024736A1 (ja) | 2009-08-26 | 2011-03-03 | ダイハツ工業株式会社 | プラズマアクチュエータ |
| FR2952748B1 (fr) | 2009-11-17 | 2011-12-09 | Thales Sa | Dispositif de surveillance de bon fonctionnement d'une pluralite de dispositifs, notamment d'actionneurs |
| US10011344B1 (en) * | 2009-12-31 | 2018-07-03 | Orbital Research Inc. | Plasma control and power system |
| US9975625B2 (en) * | 2010-04-19 | 2018-05-22 | The Boeing Company | Laminated plasma actuator |
| US10112700B1 (en) * | 2010-07-23 | 2018-10-30 | Orbital Research Inc. | Multi-mode mobility micro air vehicle |
| JP5700974B2 (ja) * | 2010-08-06 | 2015-04-15 | ダイハツ工業株式会社 | プラズマアクチュエータ |
| US8403271B2 (en) | 2010-08-24 | 2013-03-26 | Lockheed Martin Corporation | Passive robust flow control micro device |
| US9067674B2 (en) * | 2010-09-15 | 2015-06-30 | Saab Ab | Plasma-enhanced active laminar flow actuator system |
| US8636254B2 (en) | 2010-09-29 | 2014-01-28 | Lockheed Martin Corporation | Dynamically controlled cross flow instability inhibiting assembly |
| US9090326B2 (en) * | 2010-10-13 | 2015-07-28 | The Boeing Company | Active flow control on a vertical stabilizer and rudder |
| US8523115B2 (en) | 2011-01-28 | 2013-09-03 | Lockheed Martin Corporation | System, apparatus, program product, and related methods for providing boundary layer flow control |
| US8916795B2 (en) * | 2011-03-28 | 2014-12-23 | Lockheed Martin Corporation | Plasma actuated vortex generators |
| JP5837323B2 (ja) * | 2011-04-21 | 2015-12-24 | 株式会社東芝 | 風力発電装置 |
| KR101368448B1 (ko) * | 2011-05-02 | 2014-02-28 | 가부시끼가이샤 도시바 | 풍력 발전 시스템 및 그 제어 방법 |
| JP5881491B2 (ja) * | 2011-05-02 | 2016-03-09 | 株式会社東芝 | 風力発電システムおよびその制御方法 |
| US20120312923A1 (en) * | 2011-06-08 | 2012-12-13 | Lockheed Martin Corporation | Mitigating transonic shock wave with plasma heating elements |
| CN102756803B (zh) * | 2012-07-04 | 2015-06-17 | 北京航空航天大学 | 基于等离子体壁面射流的气动式格尼襟翼 |
| CN102887223B (zh) * | 2012-09-24 | 2015-02-11 | 北京航空航天大学 | 适用于尖后缘机翼的等离子体环量控制方法 |
| WO2014081355A1 (en) * | 2012-11-20 | 2014-05-30 | Saab Ab | An erosion protection strip for a leading edge of an airfoil article |
| KR101589596B1 (ko) * | 2013-02-01 | 2016-02-12 | 가부시끼가이샤 도시바 | 소용돌이 발생 장치 및 소용돌이 발생 방법 |
| US9820369B2 (en) | 2013-02-25 | 2017-11-14 | University Of Florida Research Foundation, Incorporated | Method and apparatus for providing high control authority atmospheric plasma |
| US20140321987A1 (en) * | 2013-03-15 | 2014-10-30 | Honeywell International Inc. | Plasma actuated cascade flow vectoring |
| JP6021703B2 (ja) * | 2013-03-21 | 2016-11-09 | 株式会社東芝 | 風力発電システム |
| JP6029068B2 (ja) * | 2013-04-30 | 2016-11-24 | 国立研究開発法人宇宙航空研究開発機構 | 表面流制御システムおよび表面流制御方法 |
| CN103287575B (zh) * | 2013-06-07 | 2016-01-13 | 上海交通大学 | 基于等离子体激励装置实现的减少表面阻力的方法 |
| CN103523208A (zh) * | 2013-10-12 | 2014-01-22 | 中国人民解放军空军工程大学 | 机翼增升装置等离子体流动控制方法 |
| US20150232172A1 (en) * | 2014-02-20 | 2015-08-20 | Donald Steve Morris | Airfoil assembly and method |
| JP6444740B2 (ja) * | 2014-05-29 | 2018-12-26 | 株式会社東芝 | 風力発電システムおよび風力発電方法 |
| EP2963241B1 (fr) * | 2014-06-30 | 2019-03-06 | Safran Aero Boosters SA | Élément de guidage de flux gazeux de turbomachine |
| CN105329437A (zh) * | 2014-08-04 | 2016-02-17 | 任军 | 垂直/水平飞行的喷口不动固定翼飞行器 |
| WO2016025699A2 (en) * | 2014-08-13 | 2016-02-18 | University Of Florida Research Foundation Inc. | Plasma actuated drag reduction |
| US10221720B2 (en) | 2014-09-03 | 2019-03-05 | Honeywell International Inc. | Structural frame integrated with variable-vectoring flow control for use in turbine systems |
| JP6403156B2 (ja) * | 2014-10-28 | 2018-10-10 | 東芝エネルギーシステムズ株式会社 | 気流発生装置、および、風力発電システム |
| US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| US11148801B2 (en) | 2017-06-27 | 2021-10-19 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| EP3363732B1 (en) | 2015-09-02 | 2020-10-14 | Jetoptera, Inc. | Ejector and airfoil configurations |
| US9725159B2 (en) | 2015-11-10 | 2017-08-08 | The Boeing Company | Mitigating shock using plasma |
| CN106564585B (zh) * | 2016-10-26 | 2019-12-10 | 北京航空航天大学 | 高性能深失速机翼结构及飞行器 |
| US10113844B1 (en) * | 2016-11-21 | 2018-10-30 | Lockheed Martin Corporation | Missile, chemical plasm steering system, and method |
| US10914559B1 (en) | 2016-11-21 | 2021-02-09 | Lockheed Martin Corporation | Missile, slot thrust attitude controller system, and method |
| US10495121B2 (en) * | 2017-11-10 | 2019-12-03 | X Development Llc | Method and apparatus for combined anemometer and plasma actuator |
| DE102017223882B4 (de) * | 2017-12-29 | 2020-07-16 | Airbus Defence and Space GmbH | Strömungsaktuatormodul und Strömungskörpersystem |
| JP6826068B2 (ja) | 2018-03-27 | 2021-02-03 | 株式会社Subaru | 流れ制御システム、流れ制御方法及び航空機 |
| JP7096698B2 (ja) * | 2018-04-23 | 2022-07-06 | 株式会社Subaru | 翼構造体、翼構造体の制御方法及び航空機 |
| JP2019189045A (ja) * | 2018-04-25 | 2019-10-31 | 株式会社Subaru | 翼構造体、翼構造体の制御方法及び航空機 |
| US10512150B2 (en) * | 2018-05-03 | 2019-12-17 | GM Global Technology Operations LLC | Systems and apparatuses for high performance atmosphere thin film piezoelectric resonant plasmas to modulate air flows |
| US11046415B1 (en) * | 2018-06-20 | 2021-06-29 | United States of Americas as represented by the Secretary of the Air Force | Multi-material printed control surface |
| US10694637B1 (en) * | 2018-09-20 | 2020-06-23 | Rockwell Collins, Inc. | Modular antenna array system with thermal management |
| JP7335765B2 (ja) * | 2019-09-30 | 2023-08-30 | 株式会社Subaru | 整流装置 |
| JP7324675B2 (ja) * | 2019-09-30 | 2023-08-10 | 株式会社Subaru | 整流装置 |
| US11905983B2 (en) * | 2020-01-23 | 2024-02-20 | Deep Science, Llc | Systems and methods for active control of surface drag using electrodes |
| 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 |
| JP2021156497A (ja) * | 2020-03-27 | 2021-10-07 | 株式会社富士通ゼネラル | 空気調和機 |
| GB2602113A (en) * | 2020-12-18 | 2022-06-22 | Airbus Operations Ltd | Stall trigger system |
| RU2769250C1 (ru) * | 2021-02-10 | 2022-03-29 | Роман Ефимович Либерзон | Способ управления сцеплением автомобиля с дорожным покрытием и устройство для его осуществления |
| 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 |
| CN113120218A (zh) * | 2021-05-25 | 2021-07-16 | 中国人民解放军空军工程大学 | 用于高亚音机翼流动分离控制的复合等离子体激励方法 |
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| US2946541A (en) * | 1955-04-11 | 1960-07-26 | John R Boyd | Airfoil fluid flow control system |
| US3095163A (en) † | 1959-10-13 | 1963-06-25 | Petroleum Res Corp | Ionized boundary layer fluid pumping system |
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| US4014168A (en) * | 1970-12-07 | 1977-03-29 | Carpenter Donald G | Electrical technique |
| US4398687A (en) * | 1981-02-25 | 1983-08-16 | The United States Of America As Represented By The Secretary Of The Navy | Thrust deflector and force augmentor |
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| US6247671B1 (en) * | 1998-09-23 | 2001-06-19 | Accurate Automation Corporation | Ion doping apparatus and method for aerodynamic flow control |
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| US6570333B1 (en) * | 2002-01-31 | 2003-05-27 | Sandia Corporation | Method for generating surface plasma |
| US6805325B1 (en) * | 2003-04-03 | 2004-10-19 | Rockwell Scientific Licensing, Llc. | Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow |
| RU2271307C2 (ru) * | 2004-05-17 | 2006-03-10 | Владимир Александрович Иванов | Способ управления аэродинамическим обтеканием летательного аппарата и генератор плазмы |
| US7413149B2 (en) * | 2004-07-21 | 2008-08-19 | United Technologies Corporation | Wing enhancement through ion entrainment of media |
| JP2009511360A (ja) | 2005-10-17 | 2009-03-19 | ベル ヘリコプター テクストロン インコーポレイテッド | 垂直離着陸航空機の翼、ナセルおよび/または胴体への抵抗低減のためのプラズマアクチュエータ |
| JP5060163B2 (ja) * | 2006-04-28 | 2012-10-31 | 株式会社東芝 | 翼 |
| US8006939B2 (en) | 2006-11-22 | 2011-08-30 | Lockheed Martin Corporation | Over-wing traveling-wave axial flow plasma accelerator |
| US7736123B2 (en) | 2006-12-15 | 2010-06-15 | General Electric Company | Plasma induced virtual turbine airfoil trailing edge extension |
-
2007
- 2007-05-25 US US11/753,857 patent/US7988101B2/en active Active
-
2008
- 2008-05-16 AT AT08156375T patent/ATE555985T1/de active
- 2008-05-16 ES ES08156375T patent/ES2387001T5/es active Active
- 2008-05-16 EP EP08156375.1A patent/EP1995171B2/en active Active
- 2008-05-21 JP JP2008133108A patent/JP5354955B2/ja active Active
- 2008-05-23 RU RU2008120780/11A patent/RU2474513C2/ru active
- 2008-05-26 CN CN2008101088067A patent/CN101332871B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| EP1995171B2 (en) | 2016-02-24 |
| JP2008290710A (ja) | 2008-12-04 |
| EP1995171B1 (en) | 2012-05-02 |
| JP5354955B2 (ja) | 2013-11-27 |
| US20090212164A1 (en) | 2009-08-27 |
| RU2474513C2 (ru) | 2013-02-10 |
| ES2387001T3 (es) | 2012-09-11 |
| EP1995171A3 (en) | 2010-12-29 |
| CN101332871B (zh) | 2013-06-26 |
| CN101332871A (zh) | 2008-12-31 |
| ATE555985T1 (de) | 2012-05-15 |
| RU2008120780A (ru) | 2009-11-27 |
| US7988101B2 (en) | 2011-08-02 |
| EP1995171A2 (en) | 2008-11-26 |
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