ATE431290T1 - Verfahren zur enteisung der eintrittskante einer aerodynamischen fläche und flugzeug mit derartigem verfahren - Google Patents

Verfahren zur enteisung der eintrittskante einer aerodynamischen fläche und flugzeug mit derartigem verfahren

Info

Publication number
ATE431290T1
ATE431290T1 AT07717868T AT07717868T ATE431290T1 AT E431290 T1 ATE431290 T1 AT E431290T1 AT 07717868 T AT07717868 T AT 07717868T AT 07717868 T AT07717868 T AT 07717868T AT E431290 T1 ATE431290 T1 AT E431290T1
Authority
AT
Austria
Prior art keywords
leading edge
iceing
aircraft
aerodynamic surface
state
Prior art date
Application number
AT07717868T
Other languages
English (en)
Inventor
Olivier Barbara
David Donjat
Original Assignee
Airbus France
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE431290T1 publication Critical patent/ATE431290T1/de

Links

Classifications

    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface
    • 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
    • B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Cleaning Of Streets, Tracks, Or Beaches (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Defrosting Systems (AREA)
  • Catalysts (AREA)
  • Paper (AREA)
AT07717868T 2006-01-16 2007-01-15 Verfahren zur enteisung der eintrittskante einer aerodynamischen fläche und flugzeug mit derartigem verfahren ATE431290T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0600350A FR2896228B1 (fr) 2006-01-16 2006-01-16 Procede de degivrage du bord d'attaque d'une surface aerodynamique et aeronef mettant en oeuvre un tel procede.
PCT/FR2007/000065 WO2007080333A1 (fr) 2006-01-16 2007-01-15 Procédé de dégivrage du bord d'attaque d'une surface aérodynamique et aéronef mettant en œuvre un tel procédé

Publications (1)

Publication Number Publication Date
ATE431290T1 true ATE431290T1 (de) 2009-05-15

Family

ID=37103024

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07717868T ATE431290T1 (de) 2006-01-16 2007-01-15 Verfahren zur enteisung der eintrittskante einer aerodynamischen fläche und flugzeug mit derartigem verfahren

Country Status (11)

Country Link
US (1) US8864078B2 (de)
EP (1) EP1973780B1 (de)
JP (1) JP5112335B2 (de)
CN (1) CN101370710B (de)
AT (1) ATE431290T1 (de)
BR (1) BRPI0706867A2 (de)
CA (1) CA2632873C (de)
DE (1) DE602007001131D1 (de)
FR (1) FR2896228B1 (de)
RU (1) RU2381962C1 (de)
WO (1) WO2007080333A1 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2954279B1 (fr) * 2009-12-18 2014-08-22 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises
GB201014244D0 (en) 2010-08-26 2010-10-13 Airbus Uk Ltd Laminar flow monitor
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
CN102900539B (zh) * 2011-07-26 2015-01-14 中航商用航空发动机有限责任公司 防冰和降噪组件
DE102012002132A1 (de) 2012-02-03 2013-08-08 Airbus Operations Gmbh Vereisungsschutzsystem für ein Flugzeug und Verfahren zum Betreiben eines Vereisungsschutzsystems
US10138811B2 (en) 2014-03-13 2018-11-27 The Boeing Company Enhanced temperature control anti-ice nozzle
JP2017136893A (ja) 2016-02-01 2017-08-10 三菱航空機株式会社 防氷装置、及び、航空機
JP6839920B2 (ja) 2016-02-12 2021-03-10 三菱航空機株式会社 防氷装置、及び、航空機
GB2547933A (en) * 2016-03-03 2017-09-06 Airbus Group Ltd Aircraft wing roughness strip
CN109823510A (zh) * 2019-03-06 2019-05-31 中南大学 高超声速飞行器及其热防护结构与冷却剂循环系统
CN111746801B (zh) * 2019-03-28 2024-10-18 庞巴迪公司 飞机机翼冰保护系统和方法
US11535386B2 (en) * 2019-06-17 2022-12-27 Pratt & Whitney Canada Corp. System and method for operating a multi-engine rotorcraft for ice accretion shedding
US11897600B2 (en) * 2019-06-28 2024-02-13 The Boeing Company Trip device for enhancing performance and handling qualities of an aircraft
TR201910265A2 (tr) 2019-07-09 2019-07-22 Karako Cem Taşima aparati
US20250346359A1 (en) * 2024-05-10 2025-11-13 The Boeing Company Engine Nacelle Inlet Having a Roughened Turbulator Surface

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1026745A (fr) * 1948-10-23 1953-04-30 Sncase Procédé de réparatition et d'écoulement d'un fluide pour échange thermique, dispositifs permettant la mise en oeuvre de ce procédé et leurs applications, en particulier aux aérodynes
US3578264A (en) * 1968-07-09 1971-05-11 Battelle Development Corp Boundary layer control of flow separation and heat exchange
FR2528384A1 (fr) * 1982-06-09 1983-12-16 Snecma Dispositif pour detecter et empecher la formation de glace sur des surfaces profilees
US5114100A (en) * 1989-12-29 1992-05-19 The Boeing Company Anti-icing system for aircraft
JPH04103497A (ja) * 1990-08-23 1992-04-06 Mitsubishi Heavy Ind Ltd 着氷防止装置
US5248116A (en) * 1992-02-07 1993-09-28 The B. F. Goodrich Company Airfoil with integral de-icer using overlapped tubes
RU2083441C1 (ru) * 1992-08-28 1997-07-10 Самарское конструкторское бюро Авиационного научно-технического комплекса им.А.Н.Туполева Предкрылок самолета с воздушным обогревом
US5686003A (en) * 1994-06-06 1997-11-11 Innovative Dynamics, Inc. Shape memory alloy de-icing technology
US5590854A (en) * 1994-11-02 1997-01-07 Shatz; Solomon Movable sheet for laminar flow and deicing
US5901928A (en) * 1996-06-14 1999-05-11 Aptek, Inc. Active turbulence control technique for drag reduction
GB2324351A (en) * 1997-04-18 1998-10-21 British Aerospace Reducing drag in aircraft wing assembly
US6267328B1 (en) * 1999-10-21 2001-07-31 Rohr, Inc. Hot air injection for swirling rotational anti-icing system
US6354538B1 (en) * 1999-10-25 2002-03-12 Rohr, Inc. Passive control of hot air injection for swirling rotational type anti-icing system

Also Published As

Publication number Publication date
US20090090814A1 (en) 2009-04-09
EP1973780A1 (de) 2008-10-01
DE602007001131D1 (de) 2009-06-25
JP2009523637A (ja) 2009-06-25
CN101370710A (zh) 2009-02-18
CA2632873A1 (fr) 2007-07-19
CA2632873C (fr) 2014-08-26
FR2896228B1 (fr) 2008-02-15
FR2896228A1 (fr) 2007-07-20
EP1973780B1 (de) 2009-05-13
BRPI0706867A2 (pt) 2011-04-12
RU2381962C1 (ru) 2010-02-20
US8864078B2 (en) 2014-10-21
JP5112335B2 (ja) 2013-01-09
WO2007080333A1 (fr) 2007-07-19
CN101370710B (zh) 2012-06-27

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