[go: up one dir, main page]

WO2008006960A3 - Raccord entre pieces de matiere composite d ' un turbomoteur pour aeronef - Google Patents

Raccord entre pieces de matiere composite d ' un turbomoteur pour aeronef Download PDF

Info

Publication number
WO2008006960A3
WO2008006960A3 PCT/FR2007/001133 FR2007001133W WO2008006960A3 WO 2008006960 A3 WO2008006960 A3 WO 2008006960A3 FR 2007001133 W FR2007001133 W FR 2007001133W WO 2008006960 A3 WO2008006960 A3 WO 2008006960A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
turbine engine
jointed
overlap
fan
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/FR2007/001133
Other languages
English (en)
Other versions
WO2008006960A2 (fr
Inventor
Alain Porte
Frederic Chelin
David Lambert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
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
Priority to CA2656206A priority Critical patent/CA2656206C/fr
Priority to EP07803839A priority patent/EP2038533A2/fr
Priority to BRPI0713170-4A priority patent/BRPI0713170A2/pt
Priority to JP2009518919A priority patent/JP4982561B2/ja
Priority to US12/307,874 priority patent/US8142144B2/en
Publication of WO2008006960A2 publication Critical patent/WO2008006960A2/fr
Publication of WO2008006960A3 publication Critical patent/WO2008006960A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • F05B2260/301—Retaining bolts or nuts
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • 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
    • F05D2300/614—Fibres or filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Laminated Bodies (AREA)

Abstract

Turbomoteur (1) pour aéronef, présentant un axe longitudinal (L-L) et comportant: une entrée d'air (2), pourvue d'une paroi interne tubulaire (5); et une soufflante (3), alimentée en air par ladite entrée d'ari (2) et enfermée dans un carter, également tubulaire, l'extrémité arrière de ladite paroi interne de l'entrée d'air (2) et l'extrémité avant dudit carter de la soufflante (3) étant solidarisées l'une de l'autre à l'aide d'éléments de fixation, tels que vis, boulons ou analogue. Selon l'invention, la paroi interne (5.1 ) de l'entrée d'air (2) et le carter (12.1 ) de la soufflante (3) sont des pièces de matière composite fibres/résine, assemblées par leurs extrémités (5.1 R) et (12.1A) en regard.
PCT/FR2007/001133 2006-07-12 2007-07-04 Raccord entre pieces de matiere composite d ' un turbomoteur pour aeronef Ceased WO2008006960A2 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CA2656206A CA2656206C (fr) 2006-07-12 2007-07-04 Turbomoteur pour aeronef
EP07803839A EP2038533A2 (fr) 2006-07-12 2007-07-04 Raccord entre pieces de matiere composite d'un turbomoteur pour aeronef
BRPI0713170-4A BRPI0713170A2 (pt) 2006-07-12 2007-07-04 motor s jato para aeronave
JP2009518919A JP4982561B2 (ja) 2006-07-12 2007-07-04 航空機のタービン・エンジン
US12/307,874 US8142144B2 (en) 2006-07-12 2007-07-04 Turbine engine for aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0606336A FR2903733B1 (fr) 2006-07-12 2006-07-12 Turbomoteur pour aeronef.
FR0606336 2006-07-12

Publications (2)

Publication Number Publication Date
WO2008006960A2 WO2008006960A2 (fr) 2008-01-17
WO2008006960A3 true WO2008006960A3 (fr) 2008-03-06

Family

ID=37771030

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2007/001133 Ceased WO2008006960A2 (fr) 2006-07-12 2007-07-04 Raccord entre pieces de matiere composite d ' un turbomoteur pour aeronef

Country Status (9)

Country Link
US (1) US8142144B2 (fr)
EP (1) EP2038533A2 (fr)
JP (1) JP4982561B2 (fr)
CN (1) CN101490391A (fr)
BR (1) BRPI0713170A2 (fr)
CA (1) CA2656206C (fr)
FR (1) FR2903733B1 (fr)
RU (1) RU2398122C1 (fr)
WO (1) WO2008006960A2 (fr)

Families Citing this family (14)

* 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
FR2927953B1 (fr) * 2008-02-27 2011-08-05 Snecma Fixation de carter de turbomachine
US9140135B2 (en) * 2010-09-28 2015-09-22 United Technologies Corporation Metallic radius block for composite flange
ITMI20092102A1 (it) * 2009-11-30 2011-06-01 Vittorio Giavotto Giunzione fusibile con assorbimento di energia
FR2968364B1 (fr) * 2010-12-01 2012-12-28 Snecma Element de soufflante de turboreacteur a double flux
GB201103245D0 (en) * 2011-02-25 2011-04-13 Rolls Royce Plc A joint assembly
US8740558B2 (en) * 2011-04-29 2014-06-03 United Technologies Corporation External threaded mount attachment for fan case
CA2857938C (fr) 2011-12-07 2016-09-27 Ihi Corporation Boitier de ventilateur dote d'un bossage de fixation
EP2837775B1 (fr) 2013-08-15 2016-03-30 ALSTOM Technology Ltd Dispositif de fixation pour une turbine et procédé d'application de fixation
EP2902592B1 (fr) 2014-01-31 2017-04-12 Rolls-Royce plc Moteur à turbine à gaz
US20160061222A1 (en) * 2014-09-03 2016-03-03 Jeffrey William Robinson Composite fan housing and method
US10731507B2 (en) 2014-09-09 2020-08-04 Rolls-Royce Corporation Fan case assemblies
FR3092871B1 (fr) * 2019-02-15 2022-02-25 Airbus Operations Sas Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463124A (en) * 1945-10-01 1949-03-01 Joseph A Sims Connection for structural members
US3989984A (en) * 1975-07-11 1976-11-02 Mcdonnell Douglas Corporation Aircraft lightning protection means
GB1455235A (en) * 1974-07-10 1976-11-10 Dornier Gmbh Assembly of a member and a reinforcing insert
US4556439A (en) * 1981-09-25 1985-12-03 The Boeing Company Method of sealing and bonding laminated epoxy plates
EP0269458A1 (fr) * 1986-11-28 1988-06-01 British Aerospace Public Limited Company Dispositif de fixation parafoudre pour parties de construction d'avion en matériau composite
FR2765066A1 (fr) * 1997-06-20 1998-12-24 Aerospatiale Structure anti-etincelage, notamment pour aeronef
EP1277919A1 (fr) * 2001-07-19 2003-01-22 Rolls-Royce Plc Système de joint
EP1515005A2 (fr) * 2003-09-09 2005-03-16 Rolls-Royce Plc Système de joint en particulier pour turbosoufflante
US20050082432A1 (en) * 2003-10-21 2005-04-21 Nordman Paul S. Structural cockpit window and method of making same

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2005371B (en) * 1977-10-03 1982-06-30 Hooker Chemicals Plastics Corp Tubular device and assembly using such device in the securement of one part to another
US4232496A (en) * 1979-04-30 1980-11-11 Tridair Industries Grommet assembly for composite panels
US4834569A (en) * 1987-05-13 1989-05-30 The Boeing Company Thermal expansion compensating joint assembly
US5431532A (en) * 1994-05-20 1995-07-11 General Electric Company Blade containment system
US6327132B1 (en) 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
FR2787509B1 (fr) * 1998-12-21 2001-03-30 Aerospatiale Structure d'entree d'air pour moteur d'aeronef
GB2407344B (en) * 2003-10-22 2006-02-22 Rolls Royce Plc A liner for a gas turbine engine casing
RU2277178C2 (ru) * 2004-04-13 2006-05-27 Открытое акционерное общество "Авиадвигатель" Устройство шумоглушения в турбореактивном двухконтурном двигателе
US7246990B2 (en) * 2004-12-23 2007-07-24 General Electric Company Composite fan containment case for turbine engines

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463124A (en) * 1945-10-01 1949-03-01 Joseph A Sims Connection for structural members
GB1455235A (en) * 1974-07-10 1976-11-10 Dornier Gmbh Assembly of a member and a reinforcing insert
US3989984A (en) * 1975-07-11 1976-11-02 Mcdonnell Douglas Corporation Aircraft lightning protection means
US4556439A (en) * 1981-09-25 1985-12-03 The Boeing Company Method of sealing and bonding laminated epoxy plates
EP0269458A1 (fr) * 1986-11-28 1988-06-01 British Aerospace Public Limited Company Dispositif de fixation parafoudre pour parties de construction d'avion en matériau composite
FR2765066A1 (fr) * 1997-06-20 1998-12-24 Aerospatiale Structure anti-etincelage, notamment pour aeronef
EP1277919A1 (fr) * 2001-07-19 2003-01-22 Rolls-Royce Plc Système de joint
EP1515005A2 (fr) * 2003-09-09 2005-03-16 Rolls-Royce Plc Système de joint en particulier pour turbosoufflante
US20050082432A1 (en) * 2003-10-21 2005-04-21 Nordman Paul S. Structural cockpit window and method of making same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
MCCARTHY M. A.: "BOLTED JOINTS IN COMPOSITE AIRCRAFT STRUCTURES", COMPOSIT WORKSHOP ON JOINING AND ASSEMBLING TECHNOLOGIES, 11 April 2003 (2003-04-11), Centro Ricerche Fiat, Turin, Italy, XP002461150, Retrieved from the Internet <URL:http://www.smr.ch/bojcas/Reports/COMPOSIT-presentation.pdf> [retrieved on 20071205] *

Also Published As

Publication number Publication date
US8142144B2 (en) 2012-03-27
CA2656206C (fr) 2014-09-09
RU2398122C1 (ru) 2010-08-27
FR2903733B1 (fr) 2011-03-04
JP4982561B2 (ja) 2012-07-25
CA2656206A1 (fr) 2008-01-17
FR2903733A1 (fr) 2008-01-18
CN101490391A (zh) 2009-07-22
JP2009542973A (ja) 2009-12-03
WO2008006960A2 (fr) 2008-01-17
EP2038533A2 (fr) 2009-03-25
BRPI0713170A2 (pt) 2012-03-20
US20090290978A1 (en) 2009-11-26

Similar Documents

Publication Publication Date Title
WO2008006960A3 (fr) Raccord entre pieces de matiere composite d &#39; un turbomoteur pour aeronef
GB2434179B (en) Turbofan gas turbine engine fan rotor arrangement
WO2009087274A3 (fr) Agencement de superchargeur pour moteur à piston
WO2010033414A3 (fr) Turbocompresseur à gaz d&#39;échappement
BRPI0703627A (pt) dispositivo para silenciar um motor de turbina a gás para helicóptero, e, motor de turbina a gás para helicóptero
ATE462869T1 (de) Gasturbine
GB2454434B (en) Stator assembly including bleed ports for turbine engine compressor
WO2009077666A3 (fr) Degivrage piezo-electrique d&#39;une entree d&#39;air
WO2008043903A3 (fr) Nacelle pour turboréacteur double flux
CA2582806C (fr) Systeme et methode assurant l&#39;alimentation en air d&#39;un compresseur de turbine a gaz auxiliaire d&#39;aeronef
EP1918527A3 (fr) Ensemble moteur à turbine à gaz et et son procédé d&#39;assemblage
DE602007004959D1 (de) Abdeckstruktur für einen lufteinlass
WO2012051085A3 (fr) Turbocompresseur d&#39;échappement
GB0603030D0 (en) Gas turbine engine rotor ventilation arrangement
ATE445771T1 (de) Triebwerk für ein flugzeug
WO2008057251A3 (fr) Avion à aile fixe à bon rendement énergétique
ATE522711T1 (de) Integriertes auflademodul
RU2008100463A (ru) Турбовинтовентиляторный двигатель
EP2059679A4 (fr) Système de compresseur d&#39;air sans huile à régulateur d&#39;admission
WO2010000953A8 (fr) Nacelle pour turboreacteur
EP1884639B8 (fr) Anneau de protection contre les impacts de glace pour le carter de soufflante d&#39;un moteur d&#39;aéronef
WO2008128322A3 (fr) Diffuseur avec résistance améliorée à l&#39;érosion
GB2415749B (en) A gas turbine engine including an exhaust duct comprising a diffuser for diffusing the exhaust gas produced by the engine
GB2427659B (en) A turbofan gas turbine engine fan blade and a turbofan gas turbine engine fan rotor arrangement
WO2012027212A3 (fr) Logement de palier d&#39;un turbocompresseur de gaz d&#39;échappement

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200780026132.X

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 07803839

Country of ref document: EP

Kind code of ref document: A2

WWE Wipo information: entry into national phase

Ref document number: 2009518919

Country of ref document: JP

ENP Entry into the national phase

Ref document number: 2656206

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 12307874

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2007803839

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2009104706

Country of ref document: RU

Kind code of ref document: A

ENP Entry into the national phase

Ref document number: PI0713170

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20090109