ATE445091T1 - Luftansaugung für ein flug-tl-triebwerk - Google Patents

Luftansaugung für ein flug-tl-triebwerk

Info

Publication number
ATE445091T1
ATE445091T1 AT07803838T AT07803838T ATE445091T1 AT E445091 T1 ATE445091 T1 AT E445091T1 AT 07803838 T AT07803838 T AT 07803838T AT 07803838 T AT07803838 T AT 07803838T AT E445091 T1 ATE445091 T1 AT E445091T1
Authority
AT
Austria
Prior art keywords
air intake
airplane
engine
fibre
reinforced
Prior art date
Application number
AT07803838T
Other languages
English (en)
Inventor
Alain Porte
Jacques Lalane
Fabrice Gantie
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 ATE445091T1 publication Critical patent/ATE445091T1/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
    • 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
    • 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
    • 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
    • B64D2033/0266—Arrangement 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—Arrangement 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
  • Characterised By The Charging Evacuation (AREA)
AT07803838T 2006-07-12 2007-07-04 Luftansaugung für ein flug-tl-triebwerk ATE445091T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0606334A FR2903732B1 (fr) 2006-07-12 2006-07-12 Entree d'air pour turbomoteur d'aeronef.
PCT/FR2007/001132 WO2008006959A1 (fr) 2006-07-12 2007-07-04 Entree d'air pour turbomoteur d'aeronef

Publications (1)

Publication Number Publication Date
ATE445091T1 true ATE445091T1 (de) 2009-10-15

Family

ID=37744070

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07803838T ATE445091T1 (de) 2006-07-12 2007-07-04 Luftansaugung für ein flug-tl-triebwerk

Country Status (11)

Country Link
US (1) US20100000227A1 (de)
EP (1) EP2038532B1 (de)
JP (1) JP4837096B2 (de)
CN (1) CN101490392A (de)
AT (1) ATE445091T1 (de)
BR (1) BRPI0713172A2 (de)
CA (1) CA2656282C (de)
DE (1) DE602007002719D1 (de)
FR (1) FR2903732B1 (de)
RU (1) RU2398123C1 (de)
WO (1) WO2008006959A1 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2932233B1 (fr) * 2008-06-06 2012-09-28 Aircelle Sa Carter pour rotor de turbomachine
FR2934247A1 (fr) * 2008-07-25 2010-01-29 Snecma Nacelle de turboreacteur.
GB0907580D0 (en) * 2009-05-05 2009-06-10 Rolls Royce Plc A duct wall for a fan or a gas turbine engine
US9140135B2 (en) * 2010-09-28 2015-09-22 United Technologies Corporation Metallic radius block for composite flange
JP5847430B2 (ja) * 2011-04-26 2016-01-20 株式会社Ihi ケース、ケースの製造方法、及び成形型ユニット
JP5662566B2 (ja) * 2011-04-26 2015-02-04 株式会社Ihi 成形部品
FR2975970B1 (fr) * 2011-05-30 2013-05-17 Aircelle Sa Ensemble pour une nacelle d'aeronef
FR2978735A1 (fr) * 2011-08-05 2013-02-08 Airbus Operations Sas Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
FR2978732B1 (fr) 2011-08-05 2013-09-06 Airbus Operations Sas Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
FR2978731B1 (fr) * 2011-08-05 2014-05-02 Airbus Operations Sas Nacelle d'aeronef incorporant un anneau de renfort.
CA2857938C (en) * 2011-12-07 2016-09-27 Ihi Corporation Fan case with attachment boss
US9267691B2 (en) * 2012-01-03 2016-02-23 General Electric Company Quick disconnect combustion endcover
SG11201404100TA (en) 2012-02-16 2014-10-30 United Technologies Corp Composite fan containment case assembly
FR2998547B1 (fr) 2012-11-23 2016-01-29 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison deformable entre une entree d'air et une motorisation
FR2998548B1 (fr) * 2012-11-23 2015-01-30 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation
FR3033839B1 (fr) * 2015-03-16 2018-09-28 Safran Aircraft Engines Ensemble pour turbomachine d'aeronef comprenant un carter de soufflante equipe d'un revetement acoustique integrant un raidisseur de carter de soufflante
US20160356180A1 (en) * 2015-06-03 2016-12-08 The Boeing Company Nacelle inlet having an angle or curved aft bulkhead
FR3055885B1 (fr) * 2016-09-13 2022-06-03 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride
FR3079812A1 (fr) * 2018-04-10 2019-10-11 Airbus Operations Panneau d'attenuation acoustique pour aeronef presentant des proprietes d'absorption acoustique combinees.
FR3083214A1 (fr) * 2018-06-28 2020-01-03 Airbus Operations Nacelle d'un ensemble propulsif d'aeronef comportant une pluralite d'elements amortisseurs entre une partie avant et une partie principale, et ensemble propulsif d'aeronef associe
FR3086785B1 (fr) * 2018-09-28 2022-01-21 Airbus Operations Sas Ensemble comportant deux panneaux acoustiques juxtaposes dans lequel les panneaux comportent une face resistive qui s'etend jusqu'a une paroi d'extremite
US11371390B2 (en) * 2020-04-23 2022-06-28 Raytheon Technologies Corporation Assemblies for transferring compressive loads in flanges of composite gas turbine engine components
CN114790943A (zh) * 2021-01-25 2022-07-26 中国航发商用航空发动机有限责任公司 航空发动机短舱的进气道和航空发动机短舱
US12084982B2 (en) * 2022-10-03 2024-09-10 Rtx Corporation Flange and assembly for gas turbine engine case
BE1031981B1 (fr) * 2023-09-18 2025-04-14 Safran Aero Boosters Bride de fixation pour carter, notamment carter de compresseur basse pression, eventuellement rapide, d'une turbomachine d'aeronef

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2010434B (en) * 1977-12-16 1982-06-30 Rolls Royce Flanged joint structure for composite materials
US4534167A (en) * 1982-12-27 1985-08-13 The Boeing Company Inlet cowl attachment for jet engine
JPS62179408A (ja) * 1986-01-31 1987-08-06 富士機工株式会社 無段階シ−トリクライニング装置
JP3261664B2 (ja) * 1993-06-30 2002-03-04 新日本製鐵株式会社 繊維強化樹脂複合材中空梁の交差結合方法
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5649419A (en) * 1995-01-27 1997-07-22 The Boeing Company Rotating acoustically lined inlet splitter for a turbo-fan engine
JPH09242957A (ja) * 1996-03-08 1997-09-16 Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk 分割型繊維強化プラスチック複合材製ダクトの長手継手の締結構造およびその締結方法
DE19652172C2 (de) * 1996-12-14 1998-09-17 Daimler Benz Aerospace Airbus Druckspant für einen Flugzeugrumpf
FR2767560B1 (fr) * 1997-08-19 1999-11-12 Aerospatiale Ensemble reducteur de bruit pour turboreacteur d'aeronef
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.
FR2840647B1 (fr) * 2002-06-05 2004-10-29 Airbus France Dispositif pour le raccordement de deux pieces tubulaires de turboreacteur d'aeronef
US6920958B2 (en) * 2003-10-17 2005-07-26 The Boeing Company Annular acoustic panel
RU2267628C1 (ru) * 2004-03-25 2006-01-10 Открытое акционерное общество "Авиадвигатель" Звукопоглощающая панель для тракта турбовентиляторного двигателя
FR2868124B1 (fr) * 2004-03-29 2006-06-23 Airbus France Sas Structure d'entree d'air pour moteur d'aeronef
RU2277178C2 (ru) * 2004-04-13 2006-05-27 Открытое акционерное общество "Авиадвигатель" Устройство шумоглушения в турбореактивном двухконтурном двигателе
FR2869360B1 (fr) * 2004-04-27 2006-07-14 Airbus France Sas Ensemble reducteur de bruit pour turboreacteur d'aeronef
US7503425B2 (en) * 2006-10-02 2009-03-17 Spirit Aerosystems, Inc. Integrated inlet attachment
FI119979B (fi) * 2007-03-12 2009-05-29 Patria Aerostructures Oy Ilma-aluksen kaarielementti ja komposiittilaippa

Also Published As

Publication number Publication date
JP4837096B2 (ja) 2011-12-14
BRPI0713172A2 (pt) 2012-03-20
FR2903732A1 (fr) 2008-01-18
DE602007002719D1 (de) 2009-11-19
RU2398123C1 (ru) 2010-08-27
CA2656282A1 (fr) 2008-01-17
US20100000227A1 (en) 2010-01-07
CN101490392A (zh) 2009-07-22
EP2038532A1 (de) 2009-03-25
WO2008006959A1 (fr) 2008-01-17
EP2038532B1 (de) 2009-10-07
JP2009542972A (ja) 2009-12-03
FR2903732B1 (fr) 2008-09-12
CA2656282C (fr) 2014-09-09

Similar Documents

Publication Publication Date Title
ATE445091T1 (de) Luftansaugung für ein flug-tl-triebwerk
DE502007004583D1 (de) Leitschaufelanordnung für ein triebwerk
ATE445771T1 (de) Triebwerk für ein flugzeug
ATE481313T1 (de) Strukturelement für ein flugzeug
DE602007014391D1 (de) Propellerschaufelfixierung
BRPI0713170A2 (pt) motor s jato para aeronave
BR112014017646A8 (pt) Pré-impregnado, métodos para produzir um pré-impregnado, e de fabricação de um membro estrutural de material compósito reforçado com fibra, e, uso de um pré-impregnado
ATE553167T1 (de) Haftvermittlerschicht für verbundanordnungen
BR112014015544A2 (pt) Pré-impregnado, método de processamento de pré-impregnado e material compósito reforçado por fibra
DE602006006314D1 (de) Kanalverbindungsstück mit innenauskleidung, beschichtungsverfahren und montageverfahren
ATE515436T1 (de) Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung
WO2012123667A3 (fr) Renfort mecanique pour piece en materiau composite, notamment pour une pale d'eolienne de grandes dimensions
BR112017003641A2 (pt) palheta difusora, motor de turbina, e, método para fabricar uma palheta difusora.
ATE554913T1 (de) Verfahren zur herstellung von mehreren faserverbundbauteilen
DE602005010106D1 (de) Versteifungselement und Verfahren zu dessen Herstellung
DE602007008057D1 (de) Befestigungssystem für ein bauteil einer triebwerksgondel
ATE524521T1 (de) Zwei- oder mehrkomponentige vergussmasse
FR2933067B1 (fr) Panneau de fuselage d'aeronef renforce et procede de fabrication.
IN2014CN03058A (de)
DE602005020478D1 (de) Verfahren zur Herstellung eines zum Versteifen eines Schalenstrukturs konfigurierten länglichen Strukturelementes und Verfahren zur Herstellung eines steifen Schalenstrukturs mit wenigstens einem integrierten länglichen Versteifungselement
RU2012104779A (ru) Узел передней кромки, в частности, для воздухозаборника гондолы двигателя летательного аппарата
ATE482095T1 (de) Übergang zwischen zwei gelenkig miteinander verbundenen fahrzeugen
ATE553985T1 (de) Boden für ein motorfahrzeug
ATE524687T1 (de) Flugzeugleitungsrohr
SE0403194D0 (sv) An annular torsional rigid static component for an aircraft engine

Legal Events

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