BR112013025160A2 - dispositivo de alta elevação de uma aeronave - Google Patents
dispositivo de alta elevação de uma aeronaveInfo
- Publication number
- BR112013025160A2 BR112013025160A2 BR112013025160A BR112013025160A BR112013025160A2 BR 112013025160 A2 BR112013025160 A2 BR 112013025160A2 BR 112013025160 A BR112013025160 A BR 112013025160A BR 112013025160 A BR112013025160 A BR 112013025160A BR 112013025160 A2 BR112013025160 A2 BR 112013025160A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- lift device
- high lift
- flap
- main
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/58—Wings provided with fences or spoilers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
-
- 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
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
- Toys (AREA)
- Bridges Or Land Bridges (AREA)
Abstract
dispositivo de alta elevação de uma aeronave prevê que um dispositivo de alta elevação (3) de uma aeronave inclui: um corpo principal do flap (11) fornecido em uma parte da borda de fuga de uma asa principal (2) da aeronave de forma a ser extraído a partir de e retraído na parte da borda de fuga e se estendendo na direção de um vão giratório da asa principal (2); e uma parte suprimindo um (100, 200, 300, 400, 500, ou 600) fornecida na parte da extremidade da ponta do corpo principal do flap (11) na direção de um vão giratório do corpo principal do flap (11) e configurado para suprimir um vórtice rolando a partir de uma superfície inferior para uma parte da extremidade da ponta (11a) do corpo principal do flap(11) para a superfície superior da parte da extremidade da ponta (11a).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011074795 | 2011-03-30 | ||
JP2011-074795 | 2011-03-30 | ||
PCT/JP2012/002135 WO2012132420A1 (ja) | 2011-03-30 | 2012-03-28 | 飛行体の高揚力装置 |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112013025160A2 true BR112013025160A2 (pt) | 2017-11-14 |
BR112013025160B1 BR112013025160B1 (pt) | 2021-06-15 |
Family
ID=46930194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013025160-3A BR112013025160B1 (pt) | 2011-03-30 | 2012-03-28 | Dispositivo de hipersustentação para uma aeronave |
Country Status (6)
Country | Link |
---|---|
US (3) | US9302761B2 (pt) |
EP (1) | EP2692632B1 (pt) |
JP (1) | JP5830086B2 (pt) |
BR (1) | BR112013025160B1 (pt) |
CA (3) | CA2830352C (pt) |
WO (1) | WO2012132420A1 (pt) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5956803B2 (ja) * | 2012-03-29 | 2016-07-27 | 一般社団法人日本航空宇宙工業会 | 飛行体の高揚力装置 |
JP2016078584A (ja) * | 2014-10-15 | 2016-05-16 | 三菱航空機株式会社 | 航空機 |
WO2016097939A1 (en) * | 2014-12-18 | 2016-06-23 | Bombardier Inc. | Sound absorbers for airframe components |
JP6486201B2 (ja) * | 2015-05-28 | 2019-03-20 | 国立研究開発法人宇宙航空研究開発機構 | 翼、フラップおよび航空機 |
JP6569303B2 (ja) * | 2015-05-28 | 2019-09-04 | 三菱航空機株式会社 | フラップおよび航空機 |
FR3054714B1 (fr) * | 2016-08-01 | 2018-08-31 | Airbus Operations Sas | Procede de masquage d'un signal sonore genere par un element d'une peau d'un aeronef |
US10532805B2 (en) * | 2016-09-20 | 2020-01-14 | Gulfstream Aerospace Corporation | Airfoil for an aircraft having reduced noise generation |
DE102016123096B4 (de) | 2016-11-30 | 2023-06-22 | Airbus Defence and Space GmbH | Steuerflächenbauteil für eine Auftriebshilfevorrichtung eines Luftfahrzeugs sowie Herstellungsverfahren hierfür |
DE102018121395B4 (de) * | 2018-09-03 | 2021-06-17 | Airbus Defence and Space GmbH | Endrippenanordnung für eine Auftriebshilfevorrichtung eines Luftfahrzeugs mit Lärmminderung |
CN110920862B (zh) * | 2019-11-26 | 2022-04-08 | 中国运载火箭技术研究院 | 一种飞行器及其体襟翼 |
CN111143987B (zh) * | 2019-12-24 | 2023-08-04 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机高升力系统动力学建模方法 |
US12017754B2 (en) * | 2020-03-12 | 2024-06-25 | Textron Innovations Inc. | Download reducing wingtips |
CN112678150B (zh) * | 2020-12-31 | 2024-04-26 | 中国商用飞机有限责任公司 | 飞机后缘襟翼 |
CN112644687B (zh) * | 2020-12-31 | 2024-05-17 | 中国商用飞机有限责任公司 | 飞机后缘襟翼 |
Family Cites Families (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1767944A (en) * | 1929-03-14 | 1930-06-24 | Schleusner Henry | Aerofoil |
US2163655A (en) * | 1938-04-02 | 1939-06-27 | Charles H Zimmerman | Slotted airplane wing tip |
FR980732A (fr) * | 1943-02-15 | 1951-05-17 | Sncan | Dispositifs hypersustentateurs pour aéronefs |
GB703067A (en) * | 1950-06-09 | 1954-01-27 | Nat Res Dev | Improvements in or relating to fluid reaction flying controls for aircraft |
US3090584A (en) * | 1956-08-15 | 1963-05-21 | Power Jets Res & Dev Ltd | Aircraft |
US3578264A (en) | 1968-07-09 | 1971-05-11 | Battelle Development Corp | Boundary layer control of flow separation and heat exchange |
US3692259A (en) * | 1970-06-26 | 1972-09-19 | Shao Wen Yuan | Wing-tip vortices control |
US4131252A (en) * | 1976-06-15 | 1978-12-26 | The Boeing Company | Apparatus for compensating for airflow blockage in aircraft slotted flap assemblies |
GB2051706A (en) * | 1979-06-19 | 1981-01-21 | British Aerospace | Aircraft wings |
US4477042A (en) * | 1981-01-19 | 1984-10-16 | Griswold Ii Roger W | Vortex alleviating wing tip |
US4522360A (en) | 1983-04-27 | 1985-06-11 | Rensselaer Polytechnic Institute | Passive drag control of airfoils at transonic speeds |
JPS62299496A (ja) * | 1986-06-20 | 1987-12-26 | 三菱重工業株式会社 | 航空機用操縦舵装置 |
US5209438A (en) * | 1988-06-20 | 1993-05-11 | Israel Wygnanski | Method and apparatus for delaying the separation of flow from a solid surface |
AU6037390A (en) * | 1989-07-25 | 1991-02-22 | Hans Willi Velke | Fluid dynamic surfaces |
JPH0478793A (ja) * | 1990-07-19 | 1992-03-12 | 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 |
US5253828A (en) | 1992-07-17 | 1993-10-19 | The Board Of Regents Of The University Of Oklahoma | Concealable flap-actuated vortex generator |
GB9401691D0 (en) * | 1994-01-28 | 1994-03-23 | Hannay Ian | Foils |
US5505409A (en) * | 1994-05-20 | 1996-04-09 | Wells; Anthony R. | Supercavitating airframe |
US5749546A (en) * | 1995-07-10 | 1998-05-12 | The Boeing Company | Method and apparatus for reducing airframe aerosound |
US5806807A (en) * | 1995-10-04 | 1998-09-15 | Haney; William R. | Airfoil vortex attenuation apparatus and method |
US5927645A (en) * | 1998-01-15 | 1999-07-27 | Northrop Grumman Corporation | Shovel nose pneumatic vortex control |
RU2174483C2 (ru) * | 1998-07-13 | 2001-10-10 | Центральный аэрогидродинамический институт им. проф. Н.Е. Жуковского | Устройство для ослабления вихревого следа механизированного крыла (варианты) |
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 |
DE10020177A1 (de) * | 2000-04-25 | 2001-11-08 | Daimler Chrysler Ag | Einrichtung zur Lärmminderung an Tragflügeln von Flugzeugen |
FR2821605B1 (fr) * | 2001-03-01 | 2003-05-30 | Eads Airbus Sa | Procede et dispositif pour accelerer la destruction d'au moins deux vortex dans le sillage d'un mobile, en particulier d'un avion |
US6612524B2 (en) * | 2002-01-17 | 2003-09-02 | The Boeing Company | Forebody vortex alleviation device |
US6837465B2 (en) | 2003-01-03 | 2005-01-04 | Orbital Research Inc | Flow control device and method of controlling flow |
US20050061921A1 (en) * | 2003-09-19 | 2005-03-24 | Egolf Thomas A. | Aerodynamic tip protuberances for tip vortex intensity reduction |
US7134631B2 (en) * | 2004-06-10 | 2006-11-14 | Loth John L | Vorticity cancellation at trailing edge for induced drag elimination |
US7484930B2 (en) * | 2005-06-22 | 2009-02-03 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Noise reduction of aircraft flap |
US7475854B2 (en) * | 2005-11-21 | 2009-01-13 | The Boeing Company | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods |
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 |
BRPI0701438B1 (pt) * | 2007-04-13 | 2019-11-19 | Embraer Empresa Brasileira De Aeronautica S A | superfície de controle de aeronave em combinação em combinação com um selo aerodinâmico para redução do ruído gerado por superfícies de controle de aeronaves |
US7753316B2 (en) * | 2007-04-27 | 2010-07-13 | The Boeing Company | Deployable flap edge fence |
US7874524B2 (en) * | 2007-11-16 | 2011-01-25 | The Boeing Company | Methods and apparatus for a multi-segment flap fence |
JP5046115B2 (ja) * | 2007-12-27 | 2012-10-10 | 独立行政法人 宇宙航空研究開発機構 | 舵面端騒音低減デバイス |
DE102008027618A1 (de) * | 2008-06-10 | 2009-12-31 | Airbus Deutschland Gmbh | Vorrichtung zur Bildung von aerodynamischen Wirbeln sowie Stellklappe und Tragflügel mit einer Vorrichtung zur Bildung von aerodynamischen Wirbeln |
US8226047B2 (en) * | 2009-01-23 | 2012-07-24 | General Electric Company | Reduction of tip vortex and wake interaction effects in energy and propulsion systems |
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 |
US8695915B1 (en) * | 2011-03-11 | 2014-04-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Flap side edge liners for airframe noise reduction |
US8632031B2 (en) * | 2011-04-11 | 2014-01-21 | The Boeing Company | Systems and methods for attenuation of noise and wakes produced by aircraft |
-
2012
- 2012-03-28 US US14/008,139 patent/US9302761B2/en active Active
- 2012-03-28 CA CA2830352A patent/CA2830352C/en active Active
- 2012-03-28 JP JP2013507183A patent/JP5830086B2/ja active Active
- 2012-03-28 WO PCT/JP2012/002135 patent/WO2012132420A1/ja active Application Filing
- 2012-03-28 BR BR112013025160-3A patent/BR112013025160B1/pt active IP Right Grant
- 2012-03-28 EP EP12764943.2A patent/EP2692632B1/en active Active
- 2012-03-28 CA CA2937133A patent/CA2937133C/en active Active
- 2012-03-28 CA CA2937135A patent/CA2937135C/en active Active
-
2016
- 2016-02-24 US US15/052,472 patent/US9623956B2/en active Active
- 2016-02-24 US US15/052,497 patent/US9586672B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2937133A1 (en) | 2012-10-04 |
JP5830086B2 (ja) | 2015-12-09 |
EP2692632A1 (en) | 2014-02-05 |
US9623956B2 (en) | 2017-04-18 |
CA2937133C (en) | 2018-07-10 |
EP2692632A4 (en) | 2014-12-31 |
US20160167769A1 (en) | 2016-06-16 |
US20140014780A1 (en) | 2014-01-16 |
CA2937135C (en) | 2018-06-05 |
CA2830352C (en) | 2016-09-27 |
BR112013025160B1 (pt) | 2021-06-15 |
US20160194073A1 (en) | 2016-07-07 |
CA2830352A1 (en) | 2012-10-04 |
US9586672B2 (en) | 2017-03-07 |
US9302761B2 (en) | 2016-04-05 |
CA2937135A1 (en) | 2012-10-04 |
WO2012132420A1 (ja) | 2012-10-04 |
EP2692632B1 (en) | 2019-09-04 |
JPWO2012132420A1 (ja) | 2014-07-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112013025160A2 (pt) | dispositivo de alta elevação de uma aeronave | |
ES2646445T3 (es) | Generador de vórtice retráctil | |
BR112014002704A2 (pt) | Segmento de ponta de pá de aerogerador e método de montagem | |
DE502007005892D1 (de) | N klappenwirbel beeinflussenden vorrichtung | |
WO2009149932A3 (de) | Vorrichtung zur bildung von aerodynamischen wirbeln sowie stellklappe und tragflügel mit einer vorrichtung zur bildung von aerodynamischen wirbeln | |
ATE545580T1 (de) | Nicht planare flügelspitzenvorrichtung für flugzeugflügel und flügel mit einer solchen flügelspitzenvorrichtung | |
GB0518755D0 (en) | Wing tip device | |
MX2013014832A (es) | Tabla acuatica con remo. | |
BRPI0515409A (pt) | dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero | |
MY173536A (en) | Thin airfoil ceiling fan blade | |
IN2012DE00573A (pt) | ||
BR112014032497A2 (pt) | sistema de descarga de propante e um recipiente para uso em tal sistema de descarga de propante | |
GB2490425B (en) | Interlocking blade sheath | |
MX357626B (es) | Turbina de eje vertical. | |
ATE555983T1 (de) | Vorrichtung zur anbringung eines tragwerks an einem flugzeugrumpf | |
EP2808541A3 (en) | Wind turbine blade having a tensile-only stiffener for passive control of flap movement | |
BR112012006490A2 (pt) | inserto e ferramenta de corte com uma borda de corte | |
DE602007009720D1 (de) | Flugzeugflügel | |
BRPI1013968A8 (pt) | Dispositivo de levantamneto | |
BR112012015978A2 (pt) | articulação de engate para um veículo ferroviário, e, veículo ferroviário | |
BR112014015721A2 (pt) | porta de veículo | |
WO2011048064A3 (en) | Aircraft horizontal stabiliser fitted with leading-edge strake | |
BR112017008612A2 (pt) | ?lâmina de turbina eólica fornecida com dispositivo montado em superfície? | |
WO2009106870A3 (en) | Shock bump | |
WO2015053832A3 (en) | High-modulus coating for local stiffening of airfoil trailing edges |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 28/03/2012, OBSERVADAS AS CONDICOES LEGAIS. |