ATE428046T1 - Enteisungssystem fur die anstrímkante einer einlasshaube eines turbinentriebwerks - Google Patents

Enteisungssystem fur die anstrímkante einer einlasshaube eines turbinentriebwerks

Info

Publication number
ATE428046T1
ATE428046T1 AT06778595T AT06778595T ATE428046T1 AT E428046 T1 ATE428046 T1 AT E428046T1 AT 06778595 T AT06778595 T AT 06778595T AT 06778595 T AT06778595 T AT 06778595T AT E428046 T1 ATE428046 T1 AT E428046T1
Authority
AT
Austria
Prior art keywords
shroud
turbine engine
icing system
conduit
rear part
Prior art date
Application number
AT06778595T
Other languages
English (en)
Inventor
Alain Porte
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 ATE428046T1 publication Critical patent/ATE428046T1/de

Links

Classifications

    • 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
    • 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
    • F02C7/28—Arrangement of seals
    • 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
    • B64D2033/0206—Arrangement 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—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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sealing Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Diaphragms And Bellows (AREA)
  • Defrosting Systems (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AT06778595T 2005-06-21 2006-06-15 Enteisungssystem fur die anstrímkante einer einlasshaube eines turbinentriebwerks ATE428046T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0506264A FR2887294B1 (fr) 2005-06-21 2005-06-21 Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur

Publications (1)

Publication Number Publication Date
ATE428046T1 true ATE428046T1 (de) 2009-04-15

Family

ID=34955544

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06778595T ATE428046T1 (de) 2005-06-21 2006-06-15 Enteisungssystem fur die anstrímkante einer einlasshaube eines turbinentriebwerks

Country Status (11)

Country Link
US (1) US8308110B2 (de)
EP (1) EP1899593B1 (de)
JP (1) JP4769298B2 (de)
CN (1) CN100538047C (de)
AT (1) ATE428046T1 (de)
BR (1) BRPI0613329A2 (de)
CA (1) CA2611983C (de)
DE (1) DE602006006185D1 (de)
FR (1) FR2887294B1 (de)
RU (1) RU2365773C1 (de)
WO (1) WO2006136680A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2927882B1 (fr) * 2008-02-27 2010-02-12 Aircelle Sa Structure d'entree d'air pour une nacelle d'un aeronef
CN102099556B (zh) * 2008-07-30 2014-03-12 埃尔塞乐公司 具有气动除冰功能的用于涡轮喷气发动机舱的进气口结构
FR2935017B1 (fr) * 2008-08-13 2012-11-02 Snecma Paroi interne d'une nacelle de turbomachine
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
FR2957586B1 (fr) * 2010-03-18 2012-04-27 Airbus Operations Sas Dispositif de degivrage comprenant des moyens pour detecter une fuite au niveau d'une alimentation en air chaud
FR2961174B1 (fr) * 2010-06-10 2012-07-13 Airbus Operations Sas Dispositif de conduite d'un fluide
FR2975435B1 (fr) * 2011-05-16 2016-09-02 Snecma Dispositif de degivrage d'un bec de separation de turbomachine
GB201116337D0 (en) * 2011-09-21 2011-11-02 Airbus Operations Ltd Bleed air duct joint insulation means
US9528442B2 (en) * 2013-08-21 2016-12-27 The Boeing Company Aircraft engine anti-icing (EAI) barrier assembly, system and method
CN103672297B (zh) * 2013-12-18 2015-12-09 西南石油大学 一种非开挖地下管道保护装置
FR3021350B1 (fr) * 2014-05-20 2016-07-01 Snecma Procede de detection de fuite de fluide dans une turbomachine et systeme de distribution de fluide
BE1024684B1 (fr) * 2016-10-21 2018-05-25 Safran Aero Boosters S.A. Bec degivrant de compresseur de turbomachine axiale
FR3072421B1 (fr) * 2017-10-18 2019-09-27 Airbus Operations Levre d'entree d'air d'un moteur d'aeronef comportant un systeme de degivrage
US11408341B2 (en) * 2018-11-05 2022-08-09 Rohr, Inc. Anti-icing system for an aircraft nacelle
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
US10989116B2 (en) 2019-03-05 2021-04-27 Rohr, Inc. Inlet anti-ice double walled duct with supply line seal
US11085328B2 (en) 2019-09-09 2021-08-10 Rohr, Inc. Assembly for sealing an annular gap between an inner structure and an outer structure

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB850691A (en) * 1957-05-14 1960-10-05 Power Jets Res & Dev Ltd Improvements in or relating to aircraft engine nacelle structures
US4482114A (en) * 1981-01-26 1984-11-13 The Boeing Company Integrated thermal anti-icing and environmental control system
JPH0237034Y2 (de) * 1981-02-18 1990-10-08
US4603824A (en) * 1983-08-12 1986-08-05 The Boeing Company Wing slat anti-ice air duct system with improved slide bearings and air seal
AU581684B2 (en) * 1984-10-08 1989-03-02 Short Brothers Plc Duct for hot air
IL78786A0 (en) * 1985-06-03 1986-08-31 Short Brothers Plc Duct for hot air
SU1475257A1 (ru) * 1987-03-30 1999-07-27 С.Г. Бондарев Обогреваемое воздухоприемное устройство газотурбинного двигателя
SU1739065A1 (ru) * 1990-05-30 1992-06-07 Моторостроительное Конструкторское Бюро Г.Омск Газотурбинный двигатель
GB9120113D0 (en) * 1991-09-20 1992-09-23 Short Brothers Plc Thermal antiicing of aircraft structures
US5485975A (en) * 1994-07-19 1996-01-23 Northrop Grumman Corporation Slotted cowl inlet lip for introducing high pressure air
JP3459300B2 (ja) 1994-08-02 2003-10-20 マツダ株式会社 固体高分子型燃料電池
JPH08334018A (ja) * 1995-06-07 1996-12-17 Nissan Motor Co Ltd エンジンの二重排気管
FR2771452B1 (fr) * 1997-11-21 2000-04-14 Aerospatiale Dispositif de degivrage pour capot d'entree d'air de moteur a reaction
FR2823533B1 (fr) * 2001-04-17 2003-08-08 Eads Airbus Sa Capot d'entree d'air pour moteur a reaction, pourvu de moyens de degivrage
FR2833306A1 (fr) * 2001-12-06 2003-06-13 Aircelle Sa Dispositif de degivrage aeronautique

Also Published As

Publication number Publication date
FR2887294B1 (fr) 2007-08-10
EP1899593A1 (de) 2008-03-19
FR2887294A1 (fr) 2006-12-22
CA2611983C (fr) 2013-12-03
CN100538047C (zh) 2009-09-09
US20100200699A1 (en) 2010-08-12
DE602006006185D1 (de) 2009-05-20
JP2008544152A (ja) 2008-12-04
JP4769298B2 (ja) 2011-09-07
CA2611983A1 (fr) 2006-12-28
EP1899593B1 (de) 2009-04-08
US8308110B2 (en) 2012-11-13
BRPI0613329A2 (pt) 2011-01-04
RU2365773C1 (ru) 2009-08-27
WO2006136680A1 (fr) 2006-12-28
CN101203667A (zh) 2008-06-18

Similar Documents

Publication Publication Date Title
ATE428046T1 (de) Enteisungssystem fur die anstrímkante einer einlasshaube eines turbinentriebwerks
ATE467558T1 (de) Turbomotor mit einem system zum enteisen eines lufteinlassverkleidungsteils
DE602007007669D1 (de) Gondel für zweistromtriebwerk
DE502008000281D1 (de) Vorrichtung und verfahren zum reinigen der core engine eines strahltriebwerks
DE602007001089D1 (de) Enteisungssystem für die Nasenhaube eines Flugzeugsturbotriebwerks
WO2009060137A3 (fr) Structure d'entree d'air apte a etre montee en amont d'une structure mediane de nacelle pour moteur d'aeronef, et nacelle equipee d'une telle structure d'entree d'air
EP1801403A3 (de) Niederdruckverdichter (Booster) eines Turbofantriebwerks mit kompaktem Abblassystem
WO2009077690A3 (fr) Nacelle d'aeronef comprenant un systeme de traitement du givre optimise
ATE381482T1 (de) System zum waschen eines flugzeug-turbomotors
DE602006012202D1 (de)
DE60017063D1 (de) Heissluftabfuhrvorrichtung für die Lufteinlasshaube eines Strahltriebwerkes mit Enteisungskreislauf
DE602004001924D1 (de) Flugzeugtriebwerkscowling mit verringertem Spaltmass
DE602007003981D1 (de) Strukturgondel
BRPI0717750A2 (pt) Reversor de empuxo do tipo cascata para motor a jato e motor a jato
GB2447228B8 (en) Thermal anti-icing system
EP2484990A3 (de) Erhitzeranordnung mit abnehmbarer Erhitzereinheit
RU2008116732A (ru) Силовая установка летательного аппарата, содержащая двигатель и стойку его крепления
ATE341483T1 (de) Aufhängevorrichtung eines flugzeugtriebwerks an einem flügelpylon
WO2009097668A3 (en) Icing protection for aircraft air inlet scoops
BRPI0907478A2 (pt) flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave
RU2007145361A (ru) Система устранения обледенения передней кромки входного отверстия носового обтекателя турбинного двигателя
DE602008003915D1 (de) Hintere, untere aerodynamische verkleidung für die befestigungsvorrichtung eines flugzeugmotors
ATE507421T1 (de) Blattdichtung für turbomaschine
FI20055492A0 (fi) Järjestely ja menetelmä turbokompressorilla varustetun mäntämoottorin yhteydessä
ATE542036T1 (de) Lufteinlass eines flug-tl-triebwerks, flugzeuge mit solchen lufteinlass und verfahren zur optimierung des betriebs eines das flug-tl- triebwerks mit einem solchen lufteinlass

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties