ATE257971T1 - Herstellungsverfahren einer platte mit angepasster, schallwiederstandsfähiger schicht, sowie die hergestellte platte - Google Patents

Herstellungsverfahren einer platte mit angepasster, schallwiederstandsfähiger schicht, sowie die hergestellte platte

Info

Publication number
ATE257971T1
ATE257971T1 AT02362003T AT02362003T ATE257971T1 AT E257971 T1 ATE257971 T1 AT E257971T1 AT 02362003 T AT02362003 T AT 02362003T AT 02362003 T AT02362003 T AT 02362003T AT E257971 T1 ATE257971 T1 AT E257971T1
Authority
AT
Austria
Prior art keywords
plate
mould
resistant layer
acoustically resistant
sound
Prior art date
Application number
AT02362003T
Other languages
English (en)
Inventor
Alain Porte
Herve Batard
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 ATE257971T1 publication Critical patent/ATE257971T1/de

Links

Classifications

    • 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
    • G10K11/162—Selection of materials
    • G10K11/168—Plural layers of different materials, e.g. sandwiches
    • 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
    • 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)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Laminated Bodies (AREA)
AT02362003T 2001-03-09 2002-03-07 Herstellungsverfahren einer platte mit angepasster, schallwiederstandsfähiger schicht, sowie die hergestellte platte ATE257971T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0103227A FR2821788B1 (fr) 2001-03-09 2001-03-09 Procede de fabrication d'un panneau a couche resistive acoustique adaptee et panneau acoustique ainsi obtenu

Publications (1)

Publication Number Publication Date
ATE257971T1 true ATE257971T1 (de) 2004-01-15

Family

ID=8860925

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02362003T ATE257971T1 (de) 2001-03-09 2002-03-07 Herstellungsverfahren einer platte mit angepasster, schallwiederstandsfähiger schicht, sowie die hergestellte platte

Country Status (7)

Country Link
US (1) US6755280B2 (de)
EP (1) EP1239454B1 (de)
AT (1) ATE257971T1 (de)
CA (1) CA2373188C (de)
DE (1) DE60200164T2 (de)
ES (1) ES2214466T3 (de)
FR (1) FR2821788B1 (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
FR2847304B1 (fr) * 2002-11-18 2005-07-01 Airbus France Nacelle de reacteur d'aeronef a attenuation acoustique
CA2574108C (en) 2004-07-16 2016-05-24 Bell Helicopter Textron Inc. Counter-torque device for a helicopter
US7328771B2 (en) 2004-07-27 2008-02-12 United Technologies Corporation Zero acoustic splice fan case liner
US7314113B2 (en) * 2004-09-14 2008-01-01 Cray Inc. Acoustic absorbers for use with computer cabinet fans and other cooling systems
US7419031B2 (en) * 2005-11-04 2008-09-02 The Boeing Company Integrally damped composite aircraft floor panels
US20070022196A1 (en) * 2005-06-29 2007-01-25 Subodh Agrawal Single token multifactor authentication system and method
US7707708B2 (en) * 2005-09-21 2010-05-04 Rohr, Inc. Apparatus for making a tubular composite structure
US7520370B2 (en) * 2006-05-17 2009-04-21 William Orlin Gudim Combination acoustic diffuser and absorber and method of production thereof
US7967105B2 (en) * 2006-06-19 2011-06-28 Yen Tuan Aero-acoustic aviation engine inlet for aggressive noise abatement
US7451855B2 (en) * 2007-01-09 2008-11-18 Samw Hong Jen Wang Acoustic absorbing device
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
JP2009062977A (ja) * 2007-08-15 2009-03-26 Rohr Inc 線形音響ライナー
GB2453941B (en) * 2007-10-22 2012-01-11 Yen Tuan Aero-acoustic aviation engine inlet for aggressive noise abatement
US20090154091A1 (en) 2007-12-17 2009-06-18 Yatskov Alexander I Cooling systems and heat exchangers for cooling computer components
US8170724B2 (en) 2008-02-11 2012-05-01 Cray Inc. Systems and associated methods for controllably cooling computer components
US8245750B2 (en) 2008-02-11 2012-08-21 Rohr, Inc. Segmented mandrel for high temperature bonding of metallic axisymmetric shells having complex curvatures
FR2928415B1 (fr) * 2008-03-07 2010-12-03 Aircelle Sa Panneau acoustique d'une nacelle d'un aeronef
US7640961B2 (en) 2008-03-21 2010-01-05 Rohr, Inc. Apparatus and method for making a tubular composite barrel
US7898799B2 (en) 2008-04-01 2011-03-01 Cray Inc. Airflow management apparatus for computer cabinets and associated methods
US7903403B2 (en) 2008-10-17 2011-03-08 Cray Inc. Airflow intake systems and associated methods for use with computer cabinets
US8081459B2 (en) 2008-10-17 2011-12-20 Cray Inc. Air conditioning systems for computer systems and associated methods
US8025499B2 (en) 2008-11-03 2011-09-27 Rohr, Inc. Multi-segment tool and method for composite formation
US8472181B2 (en) 2010-04-20 2013-06-25 Cray Inc. Computer cabinets having progressive air velocity cooling systems and associated methods of manufacture and use
US20120024622A1 (en) * 2010-08-02 2012-02-02 Yen Tuan Gaseous-fluid supply system for noise abatement application
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
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly 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
DE102015113685B4 (de) 2014-11-27 2020-08-06 East-4D Carbon Technology Gmbh Luftleit- und Lärmschutzeinrichtung in einem Zweistrom-Strahltriebwerk und Verfahren zu deren Montage
GB201514363D0 (en) * 2015-08-13 2015-09-30 Rolls Royce Plc Panel for lining a gas turbine engine fan casing
US20180029719A1 (en) * 2016-07-28 2018-02-01 The Boeing Company Drag reducing liner assembly and methods of assembling the same
US10793282B2 (en) * 2016-07-28 2020-10-06 The Boeing Company Liner assembly, engine housing, and methods of assembling the same

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US3300354A (en) * 1962-04-18 1967-01-24 Whittaker Corp Method of making a filament wound sandwich core
GB1436724A (en) * 1973-06-07 1976-05-26 Bolt Beranek & Newman Reducing sound generation in fluid-flow systems embodying foil structures
GB1490923A (en) * 1975-06-23 1977-11-02 Short Brothers & Harland Ltd Sound-absorbing structures
GB2049887B (en) * 1979-05-23 1982-12-01 Coal Industry Patents Ltd Acoustic liner for attenuating noise
US4495764A (en) * 1983-05-26 1985-01-29 The United States Of America As Represented By The Secretary Of The Air Force Integrated insulation wall assembly
US4600619A (en) * 1984-12-31 1986-07-15 The Boeing Company Continuously wound filament structure for use in noise attenuation element
DE8907321U1 (de) * 1989-06-15 1991-03-28 Chlupsa, Otto, 6070 Langen, De
US5594216A (en) * 1994-11-29 1997-01-14 Lockheed Missiles & Space Co., Inc. Jet engine sound-insulation structure
FR2767411B1 (fr) * 1997-08-13 2001-11-16 Aerospatiale Couche acoustiquement resistive, procede de fabrication de cette couche et panneau acoustiquement absorbant muni d'au moins une telle couche
FR2774021B1 (fr) * 1998-01-23 2000-04-21 Aerospatiale Procede de depose simultanee par bobinage sur un support de plusieurs meches de fibres pre-impregnees, dispositif pour sa mise en oeuvre et structures en materiau composite ainsi obtenues
FR2803078B1 (fr) * 1999-12-24 2002-07-26 Aerospatiale Matra Airbus Panneau d'attenuation acoustique a couche resistive a propriete structurale et son procede d'obtention
FR2803077B1 (fr) * 1999-12-24 2002-07-26 Aerospatiale Matra Airbus Procede de realisation d'une couche acoustiquement resistive, couche resistive obtenue et paroi utilisant une telle couche
FR2815900B1 (fr) * 2000-10-31 2003-07-18 Eads Airbus Sa Panneau sandwich reducteur de bruit, notamment pour turboreacteur d'aeronef
US6439340B1 (en) * 2000-11-17 2002-08-27 Astech Manufacturing, Inc. Acoustically treated structurally reinforced sound absorbing panel
FR2817994B1 (fr) * 2000-12-08 2003-02-28 Eads Airbus Sa Panneau acoustique sandwich
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
FR2826168B1 (fr) * 2001-06-19 2003-12-05 Eads Airbus Sa Procede de realisation d'une couche acoustiquement resistive renforcee, couche resistive ainsi obtenue et panneau utilisant une telle couche

Also Published As

Publication number Publication date
FR2821788A1 (fr) 2002-09-13
CA2373188A1 (fr) 2002-09-09
ES2214466T3 (es) 2004-09-16
DE60200164D1 (de) 2004-02-19
DE60200164T2 (de) 2004-10-28
EP1239454A1 (de) 2002-09-11
US6755280B2 (en) 2004-06-29
US20020125067A1 (en) 2002-09-12
EP1239454B1 (de) 2004-01-14
CA2373188C (fr) 2010-07-06
FR2821788B1 (fr) 2004-04-02

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Legal Events

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