FR2938014B1 - Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef - Google Patents

Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef

Info

Publication number
FR2938014B1
FR2938014B1 FR0806196A FR0806196A FR2938014B1 FR 2938014 B1 FR2938014 B1 FR 2938014B1 FR 0806196 A FR0806196 A FR 0806196A FR 0806196 A FR0806196 A FR 0806196A FR 2938014 B1 FR2938014 B1 FR 2938014B1
Authority
FR
France
Prior art keywords
aircraft engine
engine nacelle
attenuation panel
acoustical attenuation
acoustical
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
FR0806196A
Other languages
English (en)
Other versions
FR2938014A1 (fr
Inventor
Guy Vauchel
Guillaume Ruckert
Edmond Szkolnik
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 FR0806196A priority Critical patent/FR2938014B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CN200980127934.9A priority patent/CN102099556B/zh
Priority to US13/056,727 priority patent/US8840059B2/en
Priority to PCT/FR2009/000934 priority patent/WO2010012899A2/fr
Priority to US13/056,822 priority patent/US8899512B2/en
Priority to BRPI0914134A priority patent/BRPI0914134A2/pt
Priority to BRPI0916330A priority patent/BRPI0916330A2/pt
Priority to RU2011106595/06A priority patent/RU2521824C2/ru
Priority to CA 2732351 priority patent/CA2732351A1/fr
Priority to CA2731974A priority patent/CA2731974A1/fr
Priority to PCT/FR2009/000935 priority patent/WO2010012900A2/fr
Priority to CN200980128501.5A priority patent/CN102301122B/zh
Priority to RU2011107174/06A priority patent/RU2545608C2/ru
Priority to EP20090784308 priority patent/EP2321510B1/fr
Priority to EP09784309A priority patent/EP2318683A2/fr
Priority to ES09784308T priority patent/ES2425078T3/es
Publication of FR2938014A1 publication Critical patent/FR2938014A1/fr
Application granted granted Critical
Publication of FR2938014B1 publication Critical patent/FR2938014B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C7/24—Heat or noise insulation
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/827—Sound absorbing structures or liners
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/22—Non-oxide ceramics
    • F05D2300/224—Carbon, e.g. graphite
    • 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
    • F05D2300/612—Foam
    • 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)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Laminated Bodies (AREA)
FR0806196A 2008-07-30 2008-11-06 Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef Expired - Fee Related FR2938014B1 (fr)

Priority Applications (16)

Application Number Priority Date Filing Date Title
FR0806196A FR2938014B1 (fr) 2008-11-06 2008-11-06 Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
PCT/FR2009/000935 WO2010012900A2 (fr) 2008-07-30 2009-07-28 Panneau d'atténuation acoustique pour nacelle de moteur d'aéronef
PCT/FR2009/000934 WO2010012899A2 (fr) 2008-07-30 2009-07-28 Ensemble de pièces reliées entre elles par un dispositif permettant de conserver l'intégrité de la surface de l'une des pièces
US13/056,822 US8899512B2 (en) 2008-07-30 2009-07-28 Acoustic attenuation panel for aircraft for engine nacelle
BRPI0914134A BRPI0914134A2 (pt) 2008-07-30 2009-07-28 conjunto de componentes e estrutura de entrada de ar
BRPI0916330A BRPI0916330A2 (pt) 2008-07-30 2009-07-28 painel de atenuação acústica para uma nacela de motor de avião, estrutura de entrada de ar, estrutura fixa interna
RU2011106595/06A RU2521824C2 (ru) 2008-07-30 2009-07-28 Узел из элементов, соединенных посредством устройства, обеспечивающего целостность поверхности одного из элементов
CA 2732351 CA2732351A1 (fr) 2008-07-30 2009-07-28 Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces
CN200980127934.9A CN102099556B (zh) 2008-07-30 2009-07-28 具有气动除冰功能的用于涡轮喷气发动机舱的进气口结构
US13/056,727 US8840059B2 (en) 2008-07-30 2009-07-28 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
CN200980128501.5A CN102301122B (zh) 2008-07-30 2009-07-28 用于飞行器发动机机舱的声衰减板
RU2011107174/06A RU2545608C2 (ru) 2008-07-30 2009-07-28 Звукоизолирующая панель, конструкция воздухозаборника и внутренняя неподвижная конструкция с такой панелью для гондолы авиадвигателя
EP20090784308 EP2321510B1 (fr) 2008-07-30 2009-07-28 Structure d'entrée d'air de nacelle de turboréacteur à dégivrage pneumatique
EP09784309A EP2318683A2 (fr) 2008-07-30 2009-07-28 Panneau d'atténuation acoustique pour nacelle de moteur d'aéronef
ES09784308T ES2425078T3 (es) 2008-07-30 2009-07-28 Estructura de entrada de aire de góndola de turborreactor con desescarchado neumático
CA2731974A CA2731974A1 (fr) 2008-07-30 2009-07-28 Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0806196A FR2938014B1 (fr) 2008-11-06 2008-11-06 Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2938014A1 FR2938014A1 (fr) 2010-05-07
FR2938014B1 true FR2938014B1 (fr) 2011-04-15

Family

ID=40466844

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0806196A Expired - Fee Related FR2938014B1 (fr) 2008-07-30 2008-11-06 Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef

Country Status (1)

Country Link
FR (1) FR2938014B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2961175B1 (fr) 2010-06-14 2013-01-04 Aircelle Sa Nacelle de turboreacteur
FR3044961B1 (fr) * 2015-12-15 2018-01-19 Safran Nacelles Panneau pour nacelle de turboreacteur comportant une protection thermique et procede de fabrication d’un tel panneau
FR3049571B1 (fr) * 2016-03-30 2019-07-12 Safran Aircraft Engines Aile d'aeronef a traitement acoustique amelioree
FR3091901B1 (fr) * 2019-01-22 2020-12-25 Safran Aircraft Engines Dispositif de réduction de bruit avec structure en nid d’abeille à perçage oblique
FR3138473A1 (fr) 2022-07-28 2024-02-02 Safran Nacelles Ensemble propulsif d’aeronef comportant un panneau de capotage ameliore

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3850261A (en) * 1973-03-01 1974-11-26 Gen Electric Wide band width single layer sound suppressing panel
FR2396868A1 (fr) * 1977-07-07 1979-02-02 Snecma Garniture insonorisante pour paroi interne de conduit de gaz, notamment de conduit de turboreacteur
US6182787B1 (en) * 1999-01-12 2001-02-06 General Electric Company Rigid sandwich panel acoustic treatment
AU1809601A (en) * 1999-12-02 2001-06-12 Touchstone Research Laboratory, Ltd. Cellular coal products and processes
ES2224807B1 (es) * 2002-08-14 2007-05-01 Sener, Ingenieria Y Sistemas, S.A. Conducto de reduccion de ruido para componentes estaticos de motores aeronauticos.
US7318499B2 (en) * 2004-02-20 2008-01-15 Honeywell International, Inc. Noise suppression structure and method of making the same

Also Published As

Publication number Publication date
FR2938014A1 (fr) 2010-05-07

Similar Documents

Publication Publication Date Title
FR2906568B1 (fr) Structure d'entree d'air deposable pour nacelle de turboreacteur.
BRPI0916330A2 (pt) painel de atenuação acústica para uma nacela de motor de avião, estrutura de entrada de ar, estrutura fixa interna
EP1879283A4 (fr) Moteur
FR2952922B1 (fr) Ensemble de manutention d'un module de moteur d'aeronef
BRPI0910935A2 (pt) desvio da nacela de motor turbojato e nacela
FR2915206B1 (fr) Compositions de lubrifiants pour biocarburants destines aux moteurs diesel.
BRPI0821504A2 (pt) nacela para motor de avião
BRPI0822363A2 (pt) Nacela de motor turbojato
FR2941673B1 (fr) Ensemble de suspension pour turboreacteur d'aeronef
EP2228523A4 (fr) Moteur marin diesel
FR2948151B1 (fr) Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef
FR2891251B1 (fr) Mat d'accrochage de moteur pour aeronef
FR2913061B1 (fr) Systeme de deshuilage pour moteur d'aeronef.
EP2034168A4 (fr) Moteur diesel pour éther diméthylique
EP2187007A4 (fr) Dispositif de commande pour moteur diesel
FR2926790B1 (fr) Systeme de guidage pour la maintenance d'une nacelle d'aeronef
FR2902830B1 (fr) Turboreacteur pour aeronef
EP2474598A4 (fr) Composition de carburant pour l'aviation
BRPI1008068A2 (pt) nacela de motor turbojato
BRPI0921772A2 (pt) nacela de motor turbojato
EP2093395B8 (fr) Structure de carter d'huile destinée à un moteur
FR2938014B1 (fr) Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
FR2934641B1 (fr) Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
FR2928347B1 (fr) Structure d'accrochage pour turboreacteur
FR2905932B1 (fr) Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

PLFP Fee payment

Year of fee payment: 12

ST Notification of lapse

Effective date: 20210706