ATE539962T1 - Eintrittskante eines flugzeuges - Google Patents

Eintrittskante eines flugzeuges

Info

Publication number
ATE539962T1
ATE539962T1 AT07858692T AT07858692T ATE539962T1 AT E539962 T1 ATE539962 T1 AT E539962T1 AT 07858692 T AT07858692 T AT 07858692T AT 07858692 T AT07858692 T AT 07858692T AT E539962 T1 ATE539962 T1 AT E539962T1
Authority
AT
Austria
Prior art keywords
leading edge
airplane
coating
treatment system
frost treatment
Prior art date
Application number
AT07858692T
Other languages
English (en)
Inventor
Fabrice Gantie
Alain Porte
Original Assignee
Airbus Operations Sas
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 Operations Sas filed Critical Airbus Operations Sas
Application granted granted Critical
Publication of ATE539962T1 publication Critical patent/ATE539962T1/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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements 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
    • 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
    • B64D15/163—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means using electro-impulsive devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Multimedia (AREA)
  • Acoustics & Sound (AREA)
  • Physics & Mathematics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Eye Examination Apparatus (AREA)
  • Defrosting Systems (AREA)
  • Braking Arrangements (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
AT07858692T 2006-11-16 2007-11-13 Eintrittskante eines flugzeuges ATE539962T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0654929A FR2908738B1 (fr) 2006-11-16 2006-11-16 Bord d'attaque d'aeronef.
PCT/FR2007/052334 WO2008059169A2 (fr) 2006-11-16 2007-11-13 Bord d'attaque d'aeronef

Publications (1)

Publication Number Publication Date
ATE539962T1 true ATE539962T1 (de) 2012-01-15

Family

ID=38017185

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07858692T ATE539962T1 (de) 2006-11-16 2007-11-13 Eintrittskante eines flugzeuges

Country Status (10)

Country Link
US (1) US8733688B2 (de)
EP (1) EP2102062B1 (de)
JP (1) JP2010510120A (de)
CN (1) CN101626953B (de)
AT (1) ATE539962T1 (de)
BR (1) BRPI0717200A2 (de)
CA (1) CA2669178A1 (de)
FR (1) FR2908738B1 (de)
RU (1) RU2467927C2 (de)
WO (1) WO2008059169A2 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2936223B1 (fr) * 2008-09-23 2010-09-17 Airbus France Dispositif de liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
FR2965249B1 (fr) 2010-09-28 2013-03-15 Eurocopter France Systeme de degivrage ameliore pour voilure fixe ou tournante d'un aeronef
FR2976556B1 (fr) * 2011-06-17 2013-12-27 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule
FR2980458B1 (fr) * 2011-09-28 2013-08-30 Aircelle Sa Ensemble de levre pour nacelle de turboreacteur a degivrage electrique
DE102014004838A1 (de) * 2014-04-02 2015-10-08 Airbus Defence and Space GmbH Effektor mit abwerfbarer Tarnschale
US9815560B2 (en) 2015-09-21 2017-11-14 General Electric Company AFT engine nacelle shape for an aircraft
US9637217B2 (en) 2015-09-21 2017-05-02 General Electric Company Aircraft having an aft engine
US9957055B2 (en) 2015-09-21 2018-05-01 General Electric Company Aft engine for an aircraft
US9884687B2 (en) 2015-09-21 2018-02-06 General Electric Company Non-axis symmetric aft engine
US9821917B2 (en) 2015-09-21 2017-11-21 General Electric Company Aft engine for an aircraft
US10017270B2 (en) 2015-10-09 2018-07-10 General Electric Company Aft engine for an aircraft
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
FR3065473B1 (fr) * 2017-04-25 2019-04-19 Airbus Operations Panneau pour le traitement acoustique comprenant des alveoles contenant chacune une pluralite de conduits
GB2563055B (en) 2017-06-01 2020-11-25 Ultra Electronics Ltd Ice protection system
IT201700067602A1 (it) * 2017-06-19 2018-12-19 Leonardo Spa Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione.
US11125157B2 (en) * 2017-09-22 2021-09-21 The Boeing Company Advanced inlet design
FR3078107B1 (fr) * 2018-02-19 2020-07-31 Safran Aircraft Engines Nacelle de turbomachine a parois acoustiquement poreuses
US10883380B2 (en) * 2018-08-24 2021-01-05 Raytheon Technologies Corporation Airfoil deicing system
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine
GB201816335D0 (en) 2018-10-08 2018-11-28 Rolls Royce Plc Sound absorber
RU2753977C1 (ru) * 2020-05-29 2021-08-25 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Способ защиты поверхностей воздухозаборника летательного аппарата от обледенения
RU2748665C1 (ru) * 2020-09-28 2021-05-28 федеральное государственное автономное образовательное учреждение высшего образования "Пермский национальный исследовательский политехнический университет" Способ удаления обледенения на аэродинамических поверхностях
CN112644714B (zh) * 2020-12-29 2022-09-09 哈尔滨工程大学 一种基于振型控制的压电振动精确除冰方法
FR3120352B1 (fr) * 2021-03-03 2024-03-08 Airbus Operations Sas Entree d’air de nacelle munie d’un système de protection contre la glace mixte
FR3123941A1 (fr) * 2021-06-15 2022-12-16 Safran Nacelles Dégivrage d’une pièce d’un aéronef

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2135119A (en) * 1935-05-11 1938-11-01 Peirce M Wood Airplane device
GB2105520A (en) * 1981-06-04 1983-03-23 Rolls Royce Electro-mechanical aircraft de-icer
US4743740A (en) * 1985-10-07 1988-05-10 Rohr Industries, Inc. Buried element deicer
US4759513A (en) * 1986-09-26 1988-07-26 Quiet Nacelle Corporation Noise reduction nacelle
JP2692134B2 (ja) * 1988-04-30 1997-12-17 株式会社島津製作所 着氷防止装置
JPH02122923A (ja) * 1988-11-01 1990-05-10 Fuji Heavy Ind Ltd 複合材パネルおよびその製造方法
US5129598A (en) * 1989-12-22 1992-07-14 B. F. Goodrich Co. Attachable electro-impulse de-icer
SU1802491A1 (ru) * 1990-05-18 1995-08-20 Московский машиностроительный завод "Скорость" Устройство для удаления льда на внешних поверхностях летательного аппарата
US6688558B2 (en) * 1999-11-23 2004-02-10 The Boeing Company Method and apparatus for aircraft inlet ice protection
JP2002167290A (ja) * 2000-11-29 2002-06-11 Ishikawajima Harima Heavy Ind Co Ltd 多孔質吸音材とその製造方法
FR2820715B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR2820716B1 (fr) 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage par circulation forcee d'un fluide, d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
JP2004034781A (ja) * 2002-07-01 2004-02-05 Ishikawajima Harima Heavy Ind Co Ltd 航空機用エンジンにおける凍結防止構造
US7588212B2 (en) * 2003-07-08 2009-09-15 Rohr Inc. Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
US7513458B2 (en) * 2005-04-22 2009-04-07 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
FR2887519B1 (fr) * 2005-06-22 2008-10-10 Airbus France Sas Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
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

Also Published As

Publication number Publication date
EP2102062A2 (de) 2009-09-23
RU2467927C2 (ru) 2012-11-27
EP2102062B1 (de) 2012-01-04
FR2908738A1 (fr) 2008-05-23
US8733688B2 (en) 2014-05-27
BRPI0717200A2 (pt) 2013-10-29
CN101626953B (zh) 2013-05-29
RU2009122730A (ru) 2010-12-27
CA2669178A1 (fr) 2008-05-22
CN101626953A (zh) 2010-01-13
FR2908738B1 (fr) 2009-12-04
WO2008059169A2 (fr) 2008-05-22
JP2010510120A (ja) 2010-04-02
WO2008059169A3 (fr) 2008-08-07
US20100294882A1 (en) 2010-11-25

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