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FR2970899B1 - Procede de fabrication d'une piece de nacelle de turboreacteur - Google Patents

Procede de fabrication d'une piece de nacelle de turboreacteur

Info

Publication number
FR2970899B1
FR2970899B1 FR1150654A FR1150654A FR2970899B1 FR 2970899 B1 FR2970899 B1 FR 2970899B1 FR 1150654 A FR1150654 A FR 1150654A FR 1150654 A FR1150654 A FR 1150654A FR 2970899 B1 FR2970899 B1 FR 2970899B1
Authority
FR
France
Prior art keywords
room
manufacturing
turboreactor
nacelle
turboreactor nacelle
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.)
Expired - Fee Related
Application number
FR1150654A
Other languages
English (en)
Other versions
FR2970899A1 (fr
Inventor
Bertrand Desjoyeaux
Olivier Hubier
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.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1150654A priority Critical patent/FR2970899B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to EP12704882.5A priority patent/EP2668025A1/fr
Priority to PCT/FR2012/050126 priority patent/WO2012101364A1/fr
Priority to BR112013016819A priority patent/BR112013016819A2/pt
Priority to CN2012800067674A priority patent/CN103338915A/zh
Priority to CA 2825116 priority patent/CA2825116A1/fr
Priority to RU2013138867/05A priority patent/RU2013138867A/ru
Publication of FR2970899A1 publication Critical patent/FR2970899A1/fr
Priority to US13/953,368 priority patent/US20140026974A1/en
Application granted granted Critical
Publication of FR2970899B1 publication Critical patent/FR2970899B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/84—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/087—Propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/748—Machines or parts thereof not otherwise provided for
    • B29L2031/7504—Turbines
    • 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)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
FR1150654A 2011-01-28 2011-01-28 Procede de fabrication d'une piece de nacelle de turboreacteur Expired - Fee Related FR2970899B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1150654A FR2970899B1 (fr) 2011-01-28 2011-01-28 Procede de fabrication d'une piece de nacelle de turboreacteur
PCT/FR2012/050126 WO2012101364A1 (fr) 2011-01-28 2012-01-20 Procédé de fabrication d'une pièce de nacelle de turboréacteur
BR112013016819A BR112013016819A2 (pt) 2011-01-28 2012-01-20 método de fabricação de um lábio de entrada de ar de nacela e lábio de entrada de ar de nacela de turbina de motor a jato
CN2012800067674A CN103338915A (zh) 2011-01-28 2012-01-20 涡轮喷气发动机舱部件的制造方法
EP12704882.5A EP2668025A1 (fr) 2011-01-28 2012-01-20 Procédé de fabrication d'une pièce de nacelle de turboréacteur
CA 2825116 CA2825116A1 (fr) 2011-01-28 2012-01-20 Procede de fabrication d'une piece de nacelle de turboreacteur
RU2013138867/05A RU2013138867A (ru) 2011-01-28 2012-01-20 Способ изготовления детали гондолы турбореактивного двигателя
US13/953,368 US20140026974A1 (en) 2011-01-28 2013-07-29 Process of manufacturing a turbojet engine nacelle part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1150654A FR2970899B1 (fr) 2011-01-28 2011-01-28 Procede de fabrication d'une piece de nacelle de turboreacteur

Publications (2)

Publication Number Publication Date
FR2970899A1 FR2970899A1 (fr) 2012-08-03
FR2970899B1 true FR2970899B1 (fr) 2014-08-22

Family

ID=45688899

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150654A Expired - Fee Related FR2970899B1 (fr) 2011-01-28 2011-01-28 Procede de fabrication d'une piece de nacelle de turboreacteur

Country Status (8)

Country Link
US (1) US20140026974A1 (fr)
EP (1) EP2668025A1 (fr)
CN (1) CN103338915A (fr)
BR (1) BR112013016819A2 (fr)
CA (1) CA2825116A1 (fr)
FR (1) FR2970899B1 (fr)
RU (1) RU2013138867A (fr)
WO (1) WO2012101364A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2988407B1 (fr) * 2012-03-22 2014-10-31 Aircelle Sa Procede de fabrication d'une preforme monobloc pour structure composite
US9725190B2 (en) * 2015-02-13 2017-08-08 The Boeing Company Aircraft engine inlet assembly apparatus
FR3092871B1 (fr) * 2019-02-15 2022-02-25 Airbus Operations Sas Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef
FR3102080B1 (fr) * 2019-10-18 2022-08-19 Safran Nacelles Procédé de réparation d’une lèvre d’entrée d’air
US12428165B2 (en) * 2023-06-05 2025-09-30 Rohr, Inc. Nacelle inlet structure with foam core

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4147822A (en) * 1976-06-24 1979-04-03 Mcdonnell Douglas Corporation Composite structure and process and apparatus for making the same
FR2740383B1 (fr) * 1995-10-27 1998-01-16 Aerospatiale Procede de fabrication d'un panneau en materiau composite avec moulage par transfert de resine
EP1764307A1 (fr) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Procédé de fabrication d'un bord d'attaque monolithique
US20100080980A1 (en) * 2008-09-30 2010-04-01 Mra Systems, Inc. Molding process for core-containing composites and composites formed thereby
FR2948098B1 (fr) * 2009-07-17 2011-07-22 Aircelle Sa Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef

Also Published As

Publication number Publication date
EP2668025A1 (fr) 2013-12-04
CN103338915A (zh) 2013-10-02
CA2825116A1 (fr) 2012-08-02
WO2012101364A1 (fr) 2012-08-02
RU2013138867A (ru) 2015-03-10
US20140026974A1 (en) 2014-01-30
FR2970899A1 (fr) 2012-08-03
BR112013016819A2 (pt) 2017-04-04

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20160930