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FR2994418B1 - Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef - Google Patents

Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef

Info

Publication number
FR2994418B1
FR2994418B1 FR1257727A FR1257727A FR2994418B1 FR 2994418 B1 FR2994418 B1 FR 2994418B1 FR 1257727 A FR1257727 A FR 1257727A FR 1257727 A FR1257727 A FR 1257727A FR 2994418 B1 FR2994418 B1 FR 2994418B1
Authority
FR
France
Prior art keywords
rail
composite material
aircraft engine
engine nacelle
sliding housing
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.)
Active
Application number
FR1257727A
Other languages
English (en)
Other versions
FR2994418A1 (fr
Inventor
Boulicaut Loic Le
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 FR1257727A priority Critical patent/FR2994418B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to BR112015001203A priority patent/BR112015001203A2/pt
Priority to CN201380042164.4A priority patent/CN104520191A/zh
Priority to PCT/FR2013/051873 priority patent/WO2014023901A1/fr
Priority to CA2879924A priority patent/CA2879924A1/fr
Priority to RU2015106638A priority patent/RU2015106638A/ru
Priority to EP13756655.0A priority patent/EP2882646A1/fr
Publication of FR2994418A1 publication Critical patent/FR2994418A1/fr
Priority to US14/611,662 priority patent/US20150152744A1/en
Application granted granted Critical
Publication of FR2994418B1 publication Critical patent/FR2994418B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • 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
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Materials Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Wind Motors (AREA)
  • Bearings For Parts Moving Linearly (AREA)
FR1257727A 2012-08-09 2012-08-09 Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef Active FR2994418B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1257727A FR2994418B1 (fr) 2012-08-09 2012-08-09 Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef
CN201380042164.4A CN104520191A (zh) 2012-08-09 2013-08-02 复合材料制成的结构部件,例如飞机发动机机舱推力反向器滑动罩的导轨
PCT/FR2013/051873 WO2014023901A1 (fr) 2012-08-09 2013-08-02 Pièce structurale en matériau composite telle qu'un rail pour capot coulissant|d'inverseur de poussée de nacelle de moteur d'aeronef
CA2879924A CA2879924A1 (fr) 2012-08-09 2013-08-02 Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef
BR112015001203A BR112015001203A2 (pt) 2012-08-09 2013-08-02 parte estrutural feita de material compósito, tal como um trilho para uma capota de um reversor de empuxo de uma nacela de motor de aeronave, montagem e nacela para um motor de aeronave.
RU2015106638A RU2015106638A (ru) 2012-08-09 2013-08-02 Конструктивная деталь из композиционного материала, такая как рельс для скользящего капота реверсора тяги гондолы двигателя летательного аппарата
EP13756655.0A EP2882646A1 (fr) 2012-08-09 2013-08-02 Pièce structurale en matériau composite telle qu'un rail pour capot coulissant d'inverseur de poussée de nacelle de moteur d'aeronef
US14/611,662 US20150152744A1 (en) 2012-08-09 2015-02-02 Structural part made of composite material such as a rail for a sliding cowl of a thrust reverser of an aircraft engine nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1257727A FR2994418B1 (fr) 2012-08-09 2012-08-09 Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2994418A1 FR2994418A1 (fr) 2014-02-14
FR2994418B1 true FR2994418B1 (fr) 2015-07-24

Family

ID=47088926

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1257727A Active FR2994418B1 (fr) 2012-08-09 2012-08-09 Piece structurale en materiau composite telle qu'un rail pour capot coulissant d'inverseur de poussee de nacelle de moteur d'aeronef

Country Status (8)

Country Link
US (1) US20150152744A1 (fr)
EP (1) EP2882646A1 (fr)
CN (1) CN104520191A (fr)
BR (1) BR112015001203A2 (fr)
CA (1) CA2879924A1 (fr)
FR (1) FR2994418B1 (fr)
RU (1) RU2015106638A (fr)
WO (1) WO2014023901A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014219068B4 (de) * 2014-09-22 2021-02-18 Premium Aerotec Gmbh Fluggasturbinenschubumkehrvorrichtung mit Führungselementen
DE102014221052A1 (de) 2014-10-16 2016-04-21 Premium Aerotec Gmbh Fluggasturbinenschubumkehrvorrichtung mit Führungsschiene
US10502074B2 (en) 2017-04-07 2019-12-10 General Electric Company Methods and assemblies for forming features in composite components
US10737444B2 (en) 2017-04-07 2020-08-11 General Electric Company Methods and assemblies for forming features in composite components
US10632650B2 (en) 2017-04-07 2020-04-28 General Electric Company Methods and assemblies for forming features in composite components
DE102019106828B4 (de) * 2019-03-18 2022-06-23 Hbpo Gmbh Vorrichtung zum Verschließen eines Kraftfahrzeugkühlmoduls
FR3116043B1 (fr) * 2020-11-09 2023-04-28 Safran Aircraft Engines Entrée d’air de nacelle d’ensemble propulsif d’aéronef pour favoriser une phase d’inversion de poussée

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372071A (en) * 1993-07-13 1994-12-13 Tracor, Inc. Thrusting separation system
FR2912189B1 (fr) * 2007-02-01 2012-02-17 Airbus France Nacelle d'aeronef incorporant un dispositif pour inverser la poussee
FR2920198B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Structure pour inverseur de poussee
FR2927310B1 (fr) * 2008-02-13 2010-07-30 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
FR2949141B1 (fr) * 2009-08-14 2011-07-15 Aircelle Sa Dispositif d'inversion de poussee
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2963949A1 (fr) * 2010-08-18 2012-02-24 Aircelle Sa Poutre notamment pour inverseur de poussee a grilles

Also Published As

Publication number Publication date
CN104520191A (zh) 2015-04-15
CA2879924A1 (fr) 2014-02-13
WO2014023901A1 (fr) 2014-02-13
FR2994418A1 (fr) 2014-02-14
RU2015106638A (ru) 2016-09-27
BR112015001203A2 (pt) 2018-06-19
EP2882646A1 (fr) 2015-06-17
US20150152744A1 (en) 2015-06-04

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