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ATE343054T1 - Schalldämpfende schicht für eine schalldämpfende platte und eine platte mit einer solchen schicht - Google Patents

Schalldämpfende schicht für eine schalldämpfende platte und eine platte mit einer solchen schicht

Info

Publication number
ATE343054T1
ATE343054T1 AT03362015T AT03362015T ATE343054T1 AT E343054 T1 ATE343054 T1 AT E343054T1 AT 03362015 T AT03362015 T AT 03362015T AT 03362015 T AT03362015 T AT 03362015T AT E343054 T1 ATE343054 T1 AT E343054T1
Authority
AT
Austria
Prior art keywords
panel
sound
layer
absorbing
splints
Prior art date
Application number
AT03362015T
Other languages
English (en)
Inventor
Alain Porte
Nathalie Pascal
Sylvain Thezelais
Eric Rambaud
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE343054T1 publication Critical patent/ATE343054T1/de

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
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • 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
    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/161—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general in systems with fluid flow
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Building Environments (AREA)
  • Laminated Bodies (AREA)
  • Exhaust Silencers (AREA)
AT03362015T 2002-09-10 2003-08-27 Schalldämpfende schicht für eine schalldämpfende platte und eine platte mit einer solchen schicht ATE343054T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0211193A FR2844304B1 (fr) 2002-09-10 2002-09-10 Couche acoustiquement resistive pour panneau d'attenuation acoustique, panneau utilisant une telle couche

Publications (1)

Publication Number Publication Date
ATE343054T1 true ATE343054T1 (de) 2006-11-15

Family

ID=31725970

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03362015T ATE343054T1 (de) 2002-09-10 2003-08-27 Schalldämpfende schicht für eine schalldämpfende platte und eine platte mit einer solchen schicht

Country Status (7)

Country Link
US (1) US6772857B2 (de)
EP (1) EP1398473B1 (de)
AT (1) ATE343054T1 (de)
CA (1) CA2439555C (de)
DE (1) DE60309112T2 (de)
ES (1) ES2274192T3 (de)
FR (1) FR2844304B1 (de)

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FR2818581B1 (fr) * 2000-12-21 2003-03-28 Eads Airbus Sa Procede de fabrication d'un panneau a couche d'amortissement acoustique protegee et panneau acoustique ainsi obtenu
FR2823590B1 (fr) * 2001-04-17 2003-07-25 Eads Airbus Sa Panneau d'attenuation acoustique comportant une couche resistive a composante structurale renforcee
FR2838860B1 (fr) * 2002-04-17 2005-01-21 Airbus France Couche acoustiquement resistive multicomposant pour panneau d'attenuation acoustique et panneau ainsi obtenu
JP2005188432A (ja) * 2003-12-26 2005-07-14 Bosch Automotive Systems Corp 燃料供給装置
US7337875B2 (en) * 2004-06-28 2008-03-04 United Technologies Corporation High admittance acoustic liner
US7328771B2 (en) * 2004-07-27 2008-02-12 United Technologies Corporation Zero acoustic splice fan case liner
US7296655B2 (en) * 2005-04-22 2007-11-20 United Technologies Corporation Duct liner acoustic splice
US7296656B2 (en) * 2005-04-22 2007-11-20 United Technologies Corporation Acoustic mechanical retainer
US7861823B2 (en) * 2005-11-04 2011-01-04 United Technologies Corporation Duct for reducing shock related noise
US8602156B2 (en) 2006-05-19 2013-12-10 United Technologies Corporation Multi-splice acoustic liner
US7967105B2 (en) * 2006-06-19 2011-06-28 Yen Tuan Aero-acoustic aviation engine inlet for aggressive noise abatement
US7866440B2 (en) * 2006-07-21 2011-01-11 Rohr, Inc. System for joining acoustic cellular panel sections in edge-to-edge relation
FR2912834B1 (fr) * 2007-02-20 2009-04-24 Airbus France Sas Procede de realisation d'une couche acoustiquement resistive d'un panneau pour le traitement acoustique
FR2912833B1 (fr) 2007-02-20 2009-08-21 Airbus France Sas Panneau pour le traitement acoustique
US20080248300A1 (en) * 2007-04-05 2008-10-09 United Technologies Corporation Processes for repairing erosion resistant coatings
FR2925463B1 (fr) * 2007-12-21 2010-04-23 Airbus France Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef
US8079443B2 (en) * 2008-01-07 2011-12-20 Pelzer Acoustic Products Gmbh Aircraft trim panel with integrated adjustable acoustic properties
GB2458679B (en) * 2008-03-28 2010-04-21 Rolls Royce Plc Acoustic liners
EP2116728A1 (de) * 2008-05-07 2009-11-11 Siemens Aktiengesellschaft Flüssigkeitsaufnahmeanordnung
DE102008051241B4 (de) 2008-10-10 2011-06-16 Airbus Operations Gmbh Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs
GB2468484A (en) * 2009-03-09 2010-09-15 Aircelle Ltd An acoustic attenuation member for an aircraft
US8424637B2 (en) * 2010-01-08 2013-04-23 Richard L. Lenz, Jr. Systems and methods for providing an asymmetric cellular acoustic diffuser
FR2966128B1 (fr) * 2010-10-15 2013-06-14 Airbus Operations Sas Nacelle d'aeronef incorporant une zone de jonction continue entre une paroi exterieure et un cadre avant et/ou un cadre arriere
DE202011001683U1 (de) 2011-01-18 2011-03-17 Pfw Aerospace Ag Schalldämmmaterial
FR2971613B1 (fr) 2011-02-10 2013-03-15 Airbus Operations Sas Panneau pour le traitement acoustique comprenant une jonction entre deux parties et procede de reparation d'un panneau pour le traitement acoustique
JP5820223B2 (ja) * 2011-10-06 2015-11-24 豊和繊維工業株式会社 自動車用防音シート及びその製造方法並びに当該防音シートを用いた自動車用ダッシュサイレンサー
FR2984280B1 (fr) * 2011-12-15 2013-12-20 Aircelle Sa Structure d'entree d'air pour nacelle de turboreacteur
EP2610052A1 (de) * 2011-12-30 2013-07-03 AGUSTAWESTLAND S.p.A. Innere Verkleidungstafel eines Luftfahrzeugs, und mit solchen Tafeln ausgestattetes Luftfahrzeug
GB2519501A (en) * 2013-08-01 2015-04-29 Rolls Royce Plc Acoustic liner
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9656761B2 (en) 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
US9708072B2 (en) 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same
US9604438B2 (en) 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
US9290274B2 (en) 2014-06-02 2016-03-22 Mra Systems, Inc. Acoustically attenuating sandwich panel constructions
US11168696B2 (en) * 2014-11-10 2021-11-09 Bascom Hunter Technologies, Inc. Vane-axial fan with a fan housing and shroud having an integral acoustic treatment including a micro-perforated panel and a plurality of compartments in an annular backspace formed by a plurality of shrouds
FR3029573B1 (fr) 2014-12-05 2019-04-05 Airbus Operations (S.A.S.) Inverseur de poussee pour un ensemble moteur d'aeronef, nacelle et ensemble moteur correspondants
EP3268550B1 (de) * 2015-03-10 2021-10-13 MRA Systems, LLC Schallauskleidungen zur verwendung in einem turbinenmotor
GB2540014B (en) * 2015-05-19 2019-01-09 Boeing Co System and method for forming elongated perforations in an inner barrel section of an engine
GB201514363D0 (en) * 2015-08-13 2015-09-30 Rolls Royce Plc Panel for lining a gas turbine engine fan casing
FR3041937B1 (fr) * 2015-10-05 2017-10-20 Airbus Operations Sas Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure
US10793282B2 (en) 2016-07-28 2020-10-06 The Boeing Company Liner assembly, engine housing, and methods of assembling the same
US10473030B2 (en) * 2017-03-07 2019-11-12 Rolls-Royce Corporation Acoustic panel of turbine engine
FR3069579B1 (fr) * 2017-07-25 2019-08-30 Safran Aircraft Engines Panneau acoustique et ensemble propulsif associe
USD843607S1 (en) * 2017-08-30 2019-03-19 Barrette Outdoor Living, Inc. Architectural screen
US11059559B2 (en) 2018-03-05 2021-07-13 General Electric Company Acoustic liners with oblique cellular structures
DE102018107096A1 (de) 2018-03-26 2019-09-26 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk und Paneel für ein Gasturbinentriebwerk
US11047304B2 (en) 2018-08-08 2021-06-29 General Electric Company Acoustic cores with sound-attenuating protuberances
US10823059B2 (en) * 2018-10-03 2020-11-03 General Electric Company Acoustic core assemblies with mechanically joined acoustic core segments, and methods of mechanically joining acoustic core segments
US11434819B2 (en) 2019-03-29 2022-09-06 General Electric Company Acoustic liners with enhanced acoustic absorption and reduced drag characteristics
FR3095674B1 (fr) * 2019-05-03 2021-04-16 Safran Aircraft Engines Grille d’inverseur de poussée incluant un traitement acoustique
FR3103953B1 (fr) * 2019-11-29 2021-11-12 Safran Aircraft Engines Pastille résonante et cellule de traitement acoustique dotée d’une telle pastille
US11668236B2 (en) 2020-07-24 2023-06-06 General Electric Company Acoustic liners with low-frequency sound wave attenuating features
FR3113170A1 (fr) * 2020-07-31 2022-02-04 Airbus Operations Matériau acoustique en bande à bride intégrée, et paroi interne d’une entrée d’air d’aéronef réalisée avec ce matériau
US11970992B2 (en) 2021-06-03 2024-04-30 General Electric Company Acoustic cores and tools and methods for forming the same
US11965425B2 (en) 2022-05-31 2024-04-23 General Electric Company Airfoil for a turbofan engine

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Also Published As

Publication number Publication date
DE60309112D1 (de) 2006-11-30
FR2844304A1 (fr) 2004-03-12
ES2274192T3 (es) 2007-05-16
CA2439555C (fr) 2011-11-15
CA2439555A1 (fr) 2004-03-10
DE60309112T2 (de) 2007-06-06
US6772857B2 (en) 2004-08-10
FR2844304B1 (fr) 2004-12-10
US20040045766A1 (en) 2004-03-11
EP1398473A1 (de) 2004-03-17
EP1398473B1 (de) 2006-10-18

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties