UA89470C2 - Устройство управления ламинарным течением и летательный аппарат, использующий подобное устройство - Google Patents
Устройство управления ламинарным течением и летательный аппарат, использующий подобное устройство Download PDFInfo
- Publication number
- UA89470C2 UA89470C2 UA20041109439A UA20041109439A UA89470C2 UA 89470 C2 UA89470 C2 UA 89470C2 UA 20041109439 A UA20041109439 A UA 20041109439A UA 20041109439 A UA20041109439 A UA 20041109439A UA 89470 C2 UA89470 C2 UA 89470C2
- Authority
- UA
- Ukraine
- Prior art keywords
- flow
- suction
- holes
- perforated
- boundary layer
- Prior art date
Links
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/22—Boundary layer controls by using a surface having multiple apertures of relatively small openings other than slots
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Laminated Bodies (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Air-Flow Control Members (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Advancing Webs (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US37365302P | 2002-04-18 | 2002-04-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| UA89470C2 true UA89470C2 (ru) | 2010-02-10 |
Family
ID=29251057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| UA20041109439A UA89470C2 (ru) | 2002-04-18 | 2003-04-17 | Устройство управления ламинарным течением и летательный аппарат, использующий подобное устройство |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US7152829B2 (ru) |
| EP (1) | EP1578663B1 (ru) |
| JP (2) | JP4268886B2 (ru) |
| CN (1) | CN100408429C (ru) |
| AU (1) | AU2003230975A1 (ru) |
| BR (1) | BR0309313B1 (ru) |
| CA (2) | CA2482247C (ru) |
| RU (1) | RU2324625C2 (ru) |
| UA (1) | UA89470C2 (ru) |
| WO (1) | WO2003089295A2 (ru) |
Families Citing this family (61)
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| DE10024624A1 (de) * | 2000-05-18 | 2001-11-22 | Bayer Ag | Modifizierte Polyisocyanate |
| ATE497911T1 (de) * | 2005-08-02 | 2011-02-15 | Univ Stuttgart | Strömungsoberfläche für dreidimensionelle grenzschichtsströmung, insbesondere an einem gepfeilten flügel, einem gepfeilten leitwerk oder einem rotor |
| US7923668B2 (en) * | 2006-02-24 | 2011-04-12 | Rohr, Inc. | Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
| US7291815B2 (en) | 2006-02-24 | 2007-11-06 | Goodrich Corporation | Composite ice protection heater and method of producing same |
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| CN101565893B (zh) | 2006-05-02 | 2015-05-20 | 罗尔股份有限公司 | 制造纳米增强碳纤维和含有纳米增强碳纤维的组件的方法 |
| DE102006049616B4 (de) * | 2006-10-20 | 2010-08-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Anordnung eines Aerodynamischen Bauteils mit einer geschlitzten Hinter- oder Seitenkante in einer Strömung |
| US20080166563A1 (en) | 2007-01-04 | 2008-07-10 | Goodrich Corporation | Electrothermal heater made from thermally conducting electrically insulating polymer material |
| US7850126B2 (en) * | 2007-04-25 | 2010-12-14 | The Boeing Company | Laminar flow surfaces with selected roughness distributions, and associated methods |
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| US20090002463A1 (en) * | 2007-06-29 | 2009-01-01 | Jinquan Xu | Perforated fluid flow device for printing system |
| WO2011149440A2 (en) * | 2007-08-02 | 2011-12-01 | Sinhatech | Method for enhancing flow drag reduction and lift generation with a deturbulator |
| WO2009045559A1 (en) * | 2007-10-05 | 2009-04-09 | Oxford Aero Equipment, Llc | Surface ventilator for a compliant-surface flow-control device |
| US20090210103A1 (en) * | 2007-12-03 | 2009-08-20 | Mr. Michael Cook | Controlling aircraft aerial movements, defeating icing on aircraft surfaces, aiding decontamination, and damping turbulence effects on aircraft by the method of micro-perforated airfoil coordinated precision flow management |
| US7837150B2 (en) * | 2007-12-21 | 2010-11-23 | Rohr, Inc. | Ice protection system for a multi-segment aircraft component |
| GB2467130B (en) * | 2009-01-22 | 2012-11-28 | Cav Advanced Technologies Ltd | Method for perforating material |
| CN101602404B (zh) * | 2009-07-03 | 2013-12-25 | 朱晓义 | 一种新型结构的飞行器 |
| US8870124B2 (en) * | 2009-07-10 | 2014-10-28 | Peter Ireland | Application of elastomeric vortex generators |
| US8561934B2 (en) | 2009-08-28 | 2013-10-22 | Teresa M. Kruckenberg | Lightning strike protection |
| DE102009043489A1 (de) | 2009-09-30 | 2011-03-31 | Airbus Operations Gmbh | Vorrichtung zur Grenzschichtabsaugung und Verbundbauteil hierfür |
| DE102009049049A1 (de) * | 2009-10-12 | 2011-04-14 | Airbus Operations Gmbh | Strömungskörper insbesondere für Luftfahrzeuge |
| GB0919110D0 (en) * | 2009-11-02 | 2009-12-16 | Rolls Royce Plc | A boundary layer energiser |
| US10556670B2 (en) | 2010-08-15 | 2020-02-11 | The Boeing Company | Laminar flow panel |
| US8783624B2 (en) | 2010-08-15 | 2014-07-22 | The Boeing Company | Laminar flow panel |
| US8974177B2 (en) * | 2010-09-28 | 2015-03-10 | United Technologies Corporation | Nacelle with porous surfaces |
| 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 |
| US8919127B2 (en) | 2011-05-24 | 2014-12-30 | General Electric Company | System and method for flow control in gas turbine engine |
| EP2644497B1 (en) * | 2012-03-29 | 2016-01-20 | Airbus Operations GmbH | Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift |
| EP2644496B1 (en) * | 2012-03-29 | 2015-07-01 | Airbus Operations GmbH | Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element |
| WO2014120328A2 (en) * | 2012-11-19 | 2014-08-07 | The Regents Of The University Of California | Hypersonic laminar flow control |
| US9487288B2 (en) * | 2013-06-04 | 2016-11-08 | The Boeing Company | Apparatus and methods for extending hybrid laminar flow control |
| DE102013111175B3 (de) * | 2013-10-09 | 2014-09-04 | Dr. Schneider Kunststoffwerke Gmbh | Luftausströmer |
| US10072511B2 (en) | 2014-10-02 | 2018-09-11 | Rolls-Royce North American Technologies Inc. | Engine nacelle |
| EP3216927A4 (en) | 2014-11-05 | 2018-08-01 | Volvo Construction Equipment AB | Driving straight ahead device for construction machine and control method therefor |
| CN104386236A (zh) | 2014-11-17 | 2015-03-04 | 朱晓义 | 具有更大升力的飞行器 |
| US10000293B2 (en) | 2015-01-23 | 2018-06-19 | General Electric Company | Gas-electric propulsion system for an aircraft |
| US9932481B2 (en) * | 2015-04-21 | 2018-04-03 | The Boeing Company | Actuatable microstructures and methods of making the same |
| US9482096B1 (en) * | 2015-04-28 | 2016-11-01 | The Boeing Company | Textured leading edge for aerospace and nautical structures |
| GB201508545D0 (en) * | 2015-05-19 | 2015-07-01 | Rolls Royce Plc | Compressor tip injector |
| FR3037318B1 (fr) * | 2015-06-15 | 2017-06-30 | Snecma | Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage |
| US10279899B2 (en) * | 2015-07-02 | 2019-05-07 | Blr Aerospace L.L.C. | Helicopter with anti-torque system, related kit and methods |
| US20170198988A1 (en) * | 2016-01-13 | 2017-07-13 | Hamilton Sundstrand Corporation | Vanes for heat exchangers |
| GB2556110B (en) * | 2016-11-21 | 2020-04-01 | Dyson Technology Ltd | Compressor blade surface patterning |
| GB2557341A (en) | 2016-12-07 | 2018-06-20 | Airbus Operations Ltd | Aircraft wing assembly |
| RU2657592C1 (ru) * | 2017-03-23 | 2018-06-14 | Юрий Петрович Андреев | Способ создания движущей силы летательного аппарата |
| WO2018196810A1 (zh) | 2017-04-26 | 2018-11-01 | 朱晓义 | 从流体连续性中获得更大推动力和升力的飞行器 |
| CN107150788A (zh) * | 2017-04-26 | 2017-09-12 | 朱晓义 | 一种产生更大升力的固定翼飞行器 |
| CN107089327A (zh) * | 2017-04-26 | 2017-08-25 | 朱晓义 | 一种产生更大升力的飞行器 |
| GB2561880A (en) | 2017-04-27 | 2018-10-31 | Airbus Operations Ltd | Aerodynamic body |
| CN106949120A (zh) * | 2017-05-05 | 2017-07-14 | 吉林大学 | 一种仿生抗冲蚀管道 |
| EP3428062A1 (en) * | 2017-07-11 | 2019-01-16 | Airbus Operations GmbH | A leading edge structure for a flow control system of an aircraft |
| JP7412774B2 (ja) | 2017-12-22 | 2024-01-15 | オーチャライ ミカエル | 粘性抗力低減クラッド |
| GB2571542A (en) | 2018-02-28 | 2019-09-04 | Airbus Operations Ltd | Apparatus and method for heating an aircraft structure |
| WO2020041509A1 (en) | 2018-08-24 | 2020-02-27 | Quest Engines, LLC | Controlled turbulence system |
| GB2581974A (en) * | 2019-03-05 | 2020-09-09 | Airbus Operations Ltd | Aerofoil leading edge structures |
| CN110481761B (zh) * | 2019-08-20 | 2021-07-13 | 空气动力学国家重点实验室 | 一种利用表面开孔/槽的流动转捩被动控制装置 |
| GB2588830A (en) | 2019-11-11 | 2021-05-12 | Airbus Operations Ltd | Active drag control system for an aircraft |
| US12109793B2 (en) | 2019-11-21 | 2024-10-08 | Rtx Corporation | Composite skins having variable hole sizes and shapes formed using photomachining |
| CN112208748B (zh) * | 2020-10-13 | 2022-10-11 | 中国人民解放军国防科技大学 | 一种主被动组合的超高速边界层转捩宽频控制方法 |
| CN113483983B (zh) * | 2021-09-08 | 2021-11-16 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种孔壁横流特性测定装置及其测定方法 |
| CN115783233B (zh) * | 2023-02-09 | 2023-04-21 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种基于波纹壁及边界层抽吸的组合式转捩控制装置 |
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| US2646945A (en) * | 1950-09-05 | 1953-07-28 | John A Perry | Airplane wing structure |
| US2742247A (en) * | 1950-10-31 | 1956-04-17 | Handley Page Ltd | Outer surfaces for craft moving in one fluid |
| US2833492A (en) * | 1955-02-07 | 1958-05-06 | Harlan D Fowler | Boundary layer control system with aerodynamic glove |
| US3203648A (en) | 1961-12-26 | 1965-08-31 | Northrop Corp | Means for removing boundary layer air from aircraft |
| US3261576A (en) * | 1962-06-14 | 1966-07-19 | Olin Mathieson | Aircraft structure |
| GB1125121A (en) * | 1964-10-20 | 1968-08-28 | Joseph Brian Edwards | Improvements in or relating to aircraft aerodynamic structures |
| DE1268979B (de) * | 1966-07-01 | 1968-05-22 | Hermann Papst | UEberstroemte Wand, insbesondere bei Luftfahrzeugen, mit Schlitzen zur Absaugung derGrenzschicht |
| FR2235832B1 (ru) * | 1973-07-05 | 1976-09-17 | Anxionnaz Rene | |
| JP2741224B2 (ja) * | 1988-12-16 | 1998-04-15 | 泰昭 小濱 | 境界層制御用吸い込み装置 |
| US5141182A (en) * | 1990-06-01 | 1992-08-25 | General Electric Company | Gas turbine engine fan duct base pressure drag reduction |
| US5263667A (en) | 1991-09-09 | 1993-11-23 | The Boeing Company | Perforated wing panel with variable porosity |
| JPH06191491A (ja) | 1992-07-06 | 1994-07-12 | Rockwell Internatl Corp | 層流制御に使われるタイプの穴を開けられたパネルの表面に圧力の離散領域を確立するシステム |
| GB9400577D0 (en) * | 1994-01-13 | 1994-03-09 | Britsh Aerospace Public Limite | Forming of structures |
| EP0839309B1 (en) | 1995-07-19 | 2002-03-27 | Vida, Nikolaus | Method and apparatus for controlling the boundary or wall layer of a continuous medium |
| DE19617952C2 (de) | 1996-05-04 | 1998-07-02 | Daimler Benz Aerospace Airbus | Absauggeneratorsystem eines Flugzeuges für die Laminarhaltung der Grenzschicht |
| DE19643069C2 (de) | 1996-10-18 | 1999-03-25 | Daimler Benz Aerospace Airbus | Seitenleitwerksstrukur für ein Flugzeug |
| DE19649132C2 (de) * | 1996-11-27 | 1999-09-02 | Daimler Chrysler Aerospace | Nase für eine aerodynamische Fläche und Verfahren zu ihrer Herstellung |
| US6068328A (en) * | 1997-11-25 | 2000-05-30 | Gazdzinski; Robert F. | Vehicular boundary layer control system and method |
| DE19820097C2 (de) * | 1998-05-06 | 2003-02-13 | Airbus Gmbh | Anordnung zur Grenzschichtabsaugung und Stoßgrenzschichtkontrolle für ein Flugzeug |
| DE10005348B4 (de) | 2000-02-08 | 2004-05-06 | Airbus Deutschland Gmbh | Verfahren zur Fertigung von Nasenstrukturen für aerodynamische Flächen |
| US6332593B1 (en) * | 2000-02-16 | 2001-12-25 | Brown University Research Foundation | Method and apparatus for reducing turbulent drag |
| US6866233B2 (en) * | 2003-01-03 | 2005-03-15 | Orbital Research Inc. | Reconfigurable porous technology for fluid flow control and method of controlling flow |
-
2003
- 2003-04-17 WO PCT/US2003/012008 patent/WO2003089295A2/en active Application Filing
- 2003-04-17 CN CNB038086026A patent/CN100408429C/zh not_active Expired - Fee Related
- 2003-04-17 EP EP03724090.0A patent/EP1578663B1/en not_active Expired - Lifetime
- 2003-04-17 RU RU2004133680/11A patent/RU2324625C2/ru not_active IP Right Cessation
- 2003-04-17 CA CA2482247A patent/CA2482247C/en not_active Expired - Fee Related
- 2003-04-17 AU AU2003230975A patent/AU2003230975A1/en not_active Abandoned
- 2003-04-17 US US10/511,930 patent/US7152829B2/en not_active Expired - Lifetime
- 2003-04-17 JP JP2003586022A patent/JP4268886B2/ja not_active Expired - Fee Related
- 2003-04-17 BR BRPI0309313-1A patent/BR0309313B1/pt not_active IP Right Cessation
- 2003-04-17 UA UA20041109439A patent/UA89470C2/ru unknown
- 2003-04-17 CA CA2661810A patent/CA2661810C/en not_active Expired - Fee Related
-
2008
- 2008-12-26 JP JP2008333212A patent/JP2009102007A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| CA2661810A1 (en) | 2003-10-30 |
| CN100408429C (zh) | 2008-08-06 |
| EP1578663A4 (en) | 2010-11-24 |
| WO2003089295A2 (en) | 2003-10-30 |
| EP1578663B1 (en) | 2013-06-05 |
| EP1578663A2 (en) | 2005-09-28 |
| BR0309313A (pt) | 2007-02-21 |
| US7152829B2 (en) | 2006-12-26 |
| JP4268886B2 (ja) | 2009-05-27 |
| CA2661810C (en) | 2011-05-31 |
| AU2003230975A8 (en) | 2003-11-03 |
| JP2005532209A (ja) | 2005-10-27 |
| US20050178924A1 (en) | 2005-08-18 |
| WO2003089295A3 (en) | 2005-09-15 |
| AU2003230975A1 (en) | 2003-11-03 |
| RU2324625C2 (ru) | 2008-05-20 |
| CA2482247A1 (en) | 2003-10-30 |
| BR0309313B1 (pt) | 2012-12-11 |
| JP2009102007A (ja) | 2009-05-14 |
| CN1812911A (zh) | 2006-08-02 |
| RU2004133680A (ru) | 2005-04-20 |
| CA2482247C (en) | 2010-11-09 |
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