BR112013016819A2 - 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 - Google Patents

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

Info

Publication number
BR112013016819A2
BR112013016819A2 BR112013016819A BR112013016819A BR112013016819A2 BR 112013016819 A2 BR112013016819 A2 BR 112013016819A2 BR 112013016819 A BR112013016819 A BR 112013016819A BR 112013016819 A BR112013016819 A BR 112013016819A BR 112013016819 A2 BR112013016819 A2 BR 112013016819A2
Authority
BR
Brazil
Prior art keywords
air intake
intake lip
nacelle air
making
jet engine
Prior art date
Application number
BR112013016819A
Other languages
English (en)
Inventor
Desjoyeaux Bertrand
Hubier Olivier
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
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112013016819A2 publication Critical patent/BR112013016819A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping 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
    • B29C70/48Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping 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
    • B29C70/84Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/087Propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/748Machines or parts thereof not otherwise provided for
    • B29L2031/7504Turbines
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0536Highspeed 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)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
BR112013016819A 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 BR112013016819A2 (pt)

Applications Claiming Priority (2)

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

Publications (1)

Publication Number Publication Date
BR112013016819A2 true BR112013016819A2 (pt) 2017-04-04

Family

ID=45688899

Family Applications (1)

Application Number Title Priority Date Filing Date
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

Country Status (8)

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

Families Citing this family (3)

* 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

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 (en) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Process for manufacturing a monolithic leading edge
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
RU2013138867A (ru) 2015-03-10
EP2668025A1 (fr) 2013-12-04
WO2012101364A1 (fr) 2012-08-02
FR2970899B1 (fr) 2014-08-22
CN103338915A (zh) 2013-10-02
CA2825116A1 (fr) 2012-08-02
FR2970899A1 (fr) 2012-08-03
US20140026974A1 (en) 2014-01-30

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 5A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]