ATE445771T1 - Triebwerk für ein flugzeug - Google Patents

Triebwerk für ein flugzeug

Info

Publication number
ATE445771T1
ATE445771T1 AT07803840T AT07803840T ATE445771T1 AT E445771 T1 ATE445771 T1 AT E445771T1 AT 07803840 T AT07803840 T AT 07803840T AT 07803840 T AT07803840 T AT 07803840T AT E445771 T1 ATE445771 T1 AT E445771T1
Authority
AT
Austria
Prior art keywords
rear end
flange
airplane
engine
tubular component
Prior art date
Application number
AT07803840T
Other languages
English (en)
Inventor
Alain Porte
Fabrice Gantie
Frederic Chelin
Patrick Oberle
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 ATE445771T1 publication Critical patent/ATE445771T1/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Breeding Of Plants And Reproduction By Means Of Culturing (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
AT07803840T 2006-07-12 2007-07-04 Triebwerk für ein flugzeug ATE445771T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0606337A FR2903734B1 (fr) 2006-07-12 2006-07-12 Turbomoteur pour aeronef.
PCT/FR2007/001134 WO2008006961A1 (fr) 2006-07-12 2007-07-04 Turbomoteur pour aéronef

Publications (1)

Publication Number Publication Date
ATE445771T1 true ATE445771T1 (de) 2009-10-15

Family

ID=37759967

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07803840T ATE445771T1 (de) 2006-07-12 2007-07-04 Triebwerk für ein flugzeug

Country Status (11)

Country Link
US (1) US9261021B2 (de)
EP (1) EP2038534B1 (de)
JP (1) JP5097773B2 (de)
CN (1) CN101490390B (de)
AT (1) ATE445771T1 (de)
BR (1) BRPI0713164A2 (de)
CA (1) CA2656137C (de)
DE (1) DE602007002824D1 (de)
FR (1) FR2903734B1 (de)
RU (1) RU2382218C1 (de)
WO (1) WO2008006961A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2903734B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Turbomoteur pour aeronef.
FR2926789B1 (fr) * 2008-01-29 2010-05-28 Aircelle Sa Nacelle pour turboreacteur
EP2116728A1 (de) * 2008-05-07 2009-11-11 Siemens Aktiengesellschaft Flüssigkeitsaufnahmeanordnung
FR2931205B1 (fr) 2008-05-16 2010-05-14 Aircelle Sa Ensemble propulsif pour aeronef, et structure d'entree d'air pour un tel ensemble
US8092169B2 (en) * 2008-09-16 2012-01-10 United Technologies Corporation Integrated inlet fan case
US9140135B2 (en) * 2010-09-28 2015-09-22 United Technologies Corporation Metallic radius block for composite flange
US9249082B2 (en) 2010-02-09 2016-02-02 King Abdulaziz City for Science and Technology (KACST) Synthesis of dimethyl carbonate from carbon dioxide and methanol
RU2568543C1 (ru) * 2011-12-07 2015-11-20 АйЭйчАй КОРПОРЕЙШН Крепежная бобышка и кожух вентилятора
US9534505B2 (en) 2012-07-23 2017-01-03 United Technologies Corporation Integrated nacelle inlet and metallic fan containment case
JP5945209B2 (ja) * 2012-10-25 2016-07-05 株式会社Ihi 円筒状ケース及び円筒状ケースの製造方法
FR3015593B1 (fr) * 2013-12-20 2018-09-07 Safran Aircraft Engines Carter en materiau composite a matrice organique favorisant l'evacuation des fumees

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3542152A (en) * 1968-04-08 1970-11-24 Gen Electric Sound suppression panel
US4235303A (en) * 1978-11-20 1980-11-25 The Boeing Company Combination bulk absorber-honeycomb acoustic panels
GB2054058B (en) * 1979-06-16 1983-04-20 Rolls Royce Reducing rotor noise
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
US4556439A (en) * 1981-09-25 1985-12-03 The Boeing Company Method of sealing and bonding laminated epoxy plates
US4782658A (en) * 1987-05-07 1988-11-08 Rolls-Royce Plc Deicing of a geared gas turbine engine
US6003424A (en) * 1990-03-08 1999-12-21 Alliedsignal Inc. Armor systems
US5259724A (en) * 1992-05-01 1993-11-09 General Electric Company Inlet fan blade fragment containment shield
DE4340951A1 (de) * 1992-12-04 1994-06-09 Grumman Aerospace Corp Einstückiges Triebwerkeinlaß-Schallrohr
US5431532A (en) * 1994-05-20 1995-07-11 General Electric Company Blade containment system
FR2734320B1 (fr) * 1995-05-15 1997-07-18 Aerospatiale Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
US6652222B1 (en) * 2002-09-03 2003-11-25 Pratt & Whitney Canada Corp. Fan case design with metal foam between Kevlar
DE10259943A1 (de) * 2002-12-20 2004-07-01 Rolls-Royce Deutschland Ltd & Co Kg Schutzring für das Fan-Schutzgehäuse eines Gasturbinentriebswerks
GB0403941D0 (en) * 2004-02-21 2004-03-24 Rolls Royce Plc A gas turbine engine blade containment assembly
FR2869360B1 (fr) * 2004-04-27 2006-07-14 Airbus France Sas Ensemble reducteur de bruit pour turboreacteur d'aeronef
US7328771B2 (en) * 2004-07-27 2008-02-12 United Technologies Corporation Zero acoustic splice fan case liner
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US7246990B2 (en) * 2004-12-23 2007-07-24 General Electric Company Composite fan containment case for turbine engines
FR2903734B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Turbomoteur pour aeronef.
FR2903733B1 (fr) * 2006-07-12 2011-03-04 Airbus France Turbomoteur pour aeronef.

Also Published As

Publication number Publication date
FR2903734B1 (fr) 2008-09-12
BRPI0713164A2 (pt) 2012-04-03
EP2038534A1 (de) 2009-03-25
JP2009542974A (ja) 2009-12-03
US9261021B2 (en) 2016-02-16
CA2656137C (fr) 2014-09-09
WO2008006961A1 (fr) 2008-01-17
CN101490390A (zh) 2009-07-22
JP5097773B2 (ja) 2012-12-12
EP2038534B1 (de) 2009-10-14
CA2656137A1 (fr) 2008-01-17
FR2903734A1 (fr) 2008-01-18
RU2382218C1 (ru) 2010-02-20
DE602007002824D1 (de) 2009-11-26
CN101490390B (zh) 2012-06-20
US20090255589A1 (en) 2009-10-15

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