CN101952170B - 用于飞行器前缘的空气出口系统 - Google Patents

用于飞行器前缘的空气出口系统 Download PDF

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Publication number
CN101952170B
CN101952170B CN2008801189066A CN200880118906A CN101952170B CN 101952170 B CN101952170 B CN 101952170B CN 2008801189066 A CN2008801189066 A CN 2008801189066A CN 200880118906 A CN200880118906 A CN 200880118906A CN 101952170 B CN101952170 B CN 101952170B
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CN
China
Prior art keywords
air
wedge
leading edge
shaped part
aerodynamic
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.)
Expired - Fee Related
Application number
CN2008801189066A
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English (en)
Chinese (zh)
Other versions
CN101952170A (zh
Inventor
弗雷德里克·谢兰
蒂埃里·叙尔普尔伊
克里斯托夫·布尔多
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Airbus Operations SAS
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Airbus Operations SAS
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Publication date
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Publication of CN101952170A publication Critical patent/CN101952170A/zh
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Publication of CN101952170B publication Critical patent/CN101952170B/zh
Expired - Fee Related legal-status Critical Current
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
    • 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
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
    • 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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Feedback Control In General (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Holo Graphy (AREA)
  • Braking Arrangements (AREA)
  • Body Structure For Vehicles (AREA)
CN2008801189066A 2007-12-03 2008-12-01 用于飞行器前缘的空气出口系统 Expired - Fee Related CN101952170B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0759494A FR2924407B1 (fr) 2007-12-03 2007-12-03 Systeme de sortie d'air pour un bord d'attaque d'aeronef
FR0759494 2007-12-03
PCT/FR2008/052165 WO2009077689A2 (fr) 2007-12-03 2008-12-01 Systeme de sortie d'air pour un bord d'attaque d'aeronef

Publications (2)

Publication Number Publication Date
CN101952170A CN101952170A (zh) 2011-01-19
CN101952170B true CN101952170B (zh) 2013-09-11

Family

ID=39561715

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2008801189066A Expired - Fee Related CN101952170B (zh) 2007-12-03 2008-12-01 用于飞行器前缘的空气出口系统

Country Status (10)

Country Link
US (1) US8434724B2 (enExample)
EP (1) EP2219948B1 (enExample)
JP (1) JP5672005B2 (enExample)
CN (1) CN101952170B (enExample)
AT (1) ATE520593T1 (enExample)
BR (1) BRPI0818985A2 (enExample)
CA (1) CA2707636C (enExample)
FR (1) FR2924407B1 (enExample)
RU (1) RU2485023C2 (enExample)
WO (1) WO2009077689A2 (enExample)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
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FR2924408B1 (fr) * 2007-12-03 2010-05-07 Airbus France Nacelle de turboreacteur et procede de controle du decollement dans une nacelle de turboreacteur
US20160052621A1 (en) * 2009-07-10 2016-02-25 Peter Ireland Energy efficiency improvements for turbomachinery
FR2954280B1 (fr) * 2009-12-18 2012-03-23 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef comprenant un traitement du givre optimise
JP5582927B2 (ja) * 2010-08-30 2014-09-03 三菱重工業株式会社 航空機の防除氷システム及びこれを備える航空機
FR2975972B1 (fr) * 2011-06-01 2013-11-22 Aircelle Sa Structure d'entree d'air de nacelle de turboreacteur
US20140263837A1 (en) * 2013-03-12 2014-09-18 Spirit Aerosystems, Inc. Nacelle inlet thermal anti-ice spray duct
FR3014413B1 (fr) * 2013-12-05 2018-04-20 Airbus Operations Dispositif d'ejection d'air comprenant un profil aerodynamique muni d'une languette flexible d'obturation de fente
EP2995552B1 (en) * 2014-09-09 2018-05-02 Airbus Defence and Space GmbH Chamber in an airfoil
US10072511B2 (en) 2014-10-02 2018-09-11 Rolls-Royce North American Technologies Inc. Engine nacelle
EP3090952B1 (en) 2015-03-31 2018-10-03 Rolls-Royce Corporation Engine nacelle
US10221765B2 (en) 2016-08-26 2019-03-05 Honeywell International Inc. Anti-icing exhaust system
US10655539B2 (en) * 2017-10-16 2020-05-19 Rolls-Royce North America Technologies Inc. Aircraft anti-icing system
FR3089252B1 (fr) * 2018-12-04 2022-06-24 Safran Nacelles Dispositif et procédé de dégivrage d'une entrée d'air d’une nacelle d'un turboréacteur d'aéronef
FR3092618B1 (fr) * 2019-02-08 2021-02-19 Safran Nacelles Entrée d'air d'une nacelle de turboréacteur d'aéronef comportant des ouvertures de ventilation d’un flux d’air chaud de dégivrage
FR3092619B1 (fr) 2019-02-08 2021-03-19 Safran Nacelles Entrée d'air d'une nacelle de turboréacteur d'aéronef comportant des ouvertures de ventilation d’un flux d’air chaud de dégivrage
FR3092620B1 (fr) 2019-02-08 2021-03-05 Safran Nacelles Entrée d'air d'une nacelle de turboréacteur d'aéronef comportant des ouvertures de ventilation d’un flux d’air chaud de dégivrage
FR3096662B1 (fr) * 2019-05-27 2022-08-12 Safran Nacelles Lèvre d’entrée d’air de nacelle de turbomachine comprenant un dispositif acoustique et procédé de fabrication d’une telle lèvre
FR3099915A1 (fr) * 2019-08-13 2021-02-19 Airbus Operations Partie antérieure de nacelle d’un ensemble propulsif d’aéronef dont la lèvre d’entrée d’air est liée au panneau extérieur par emboitement
CN112709637B (zh) * 2019-10-25 2022-05-10 中国航发商用航空发动机有限责任公司 提高航空发动机短舱进气道抗侧风能力的装置和方法
RU2724036C1 (ru) * 2019-11-14 2020-06-18 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Фюзеляж самолета
US11629651B2 (en) 2020-11-17 2023-04-18 General Electric Company Gas turbine engine having a turbomachine and an electric motor coupled to a propeller
CN112455693A (zh) * 2020-12-02 2021-03-09 唐建平 一种航空航天用换气装置
CN112977836B (zh) * 2021-05-11 2021-08-10 中国空气动力研究与发展中心低速空气动力研究所 一种防冰装置
CN113650791B (zh) * 2021-09-08 2022-10-25 中国商用飞机有限责任公司 一种短舱及配备有该短舱的飞行器

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5841079A (en) * 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
EP0934878A2 (en) * 1998-02-06 1999-08-11 Northrop Grumman Corporation Low drag and reduced size aircraft engine nacelle
CN1878695A (zh) * 2003-11-21 2006-12-13 空中巴士公司 飞行器的流体冷却系统和装设有这种系统的飞行器
CN1886275A (zh) * 2003-11-28 2006-12-27 邦巴尔迪尔运输有限公司 空调机组
WO2007007108A1 (en) * 2005-07-13 2007-01-18 City University An element for generating a fluid dynamic force

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3840199A (en) * 1972-05-09 1974-10-08 R Tibbs Aircraft
US3889903A (en) * 1973-03-09 1975-06-17 Boeing Co Airfoil leading edge structure with boundary layer control
US3933327A (en) * 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
US4154256A (en) * 1978-03-29 1979-05-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Self stabilizing sonic inlet
FR2528384A1 (fr) * 1982-06-09 1983-12-16 Snecma Dispositif pour detecter et empecher la formation de glace sur des surfaces profilees
US4749151A (en) * 1985-09-19 1988-06-07 The Boeing Company Apparatus for re-energizing boundary layer air
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US5934611A (en) * 1997-10-20 1999-08-10 Northrop Grumman Corporation Low drag inlet design using injected duct flow
FR2771776B1 (fr) * 1997-12-02 2000-01-28 Aerospatiale Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
US6390418B1 (en) 1999-02-25 2002-05-21 United Technologies Corporation Tangentially directed acoustic jet controlling boundary layer
RU2279998C2 (ru) * 2002-11-18 2006-07-20 Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" Воздухозаборник двигателя летательного аппарата
BRPI0611707A2 (pt) 2005-06-29 2012-04-24 Compumedics Ltd conjunto de sensor com ponte condutiva

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5841079A (en) * 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
EP0934878A2 (en) * 1998-02-06 1999-08-11 Northrop Grumman Corporation Low drag and reduced size aircraft engine nacelle
CN1878695A (zh) * 2003-11-21 2006-12-13 空中巴士公司 飞行器的流体冷却系统和装设有这种系统的飞行器
CN1886275A (zh) * 2003-11-28 2006-12-27 邦巴尔迪尔运输有限公司 空调机组
WO2007007108A1 (en) * 2005-07-13 2007-01-18 City University An element for generating a fluid dynamic force

Also Published As

Publication number Publication date
US20100327120A1 (en) 2010-12-30
WO2009077689A3 (fr) 2009-08-20
BRPI0818985A2 (pt) 2015-05-05
US8434724B2 (en) 2013-05-07
WO2009077689A2 (fr) 2009-06-25
CN101952170A (zh) 2011-01-19
CA2707636C (fr) 2015-08-04
RU2485023C2 (ru) 2013-06-20
JP2011505290A (ja) 2011-02-24
EP2219948B1 (fr) 2011-08-17
FR2924407A1 (fr) 2009-06-05
ATE520593T1 (de) 2011-09-15
RU2010127234A (ru) 2012-01-10
FR2924407B1 (fr) 2010-05-14
EP2219948A2 (fr) 2010-08-25
CA2707636A1 (fr) 2009-06-25
JP5672005B2 (ja) 2015-02-18

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Granted publication date: 20130911