ATE525285T1 - Schallbehandlungsplatte mit integrierter verbindungsverstärkung - Google Patents

Schallbehandlungsplatte mit integrierter verbindungsverstärkung

Info

Publication number
ATE525285T1
ATE525285T1 AT09742260T AT09742260T ATE525285T1 AT E525285 T1 ATE525285 T1 AT E525285T1 AT 09742260 T AT09742260 T AT 09742260T AT 09742260 T AT09742260 T AT 09742260T AT E525285 T1 ATE525285 T1 AT E525285T1
Authority
AT
Austria
Prior art keywords
treatment plate
integrated connection
connection reinforcement
panel
sound treatment
Prior art date
Application number
AT09742260T
Other languages
English (en)
Inventor
Alain Porte
Jacques Lalane
Original Assignee
Airbus Operations Sas
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 Operations Sas filed Critical Airbus Operations Sas
Application granted granted Critical
Publication of ATE525285T1 publication Critical patent/ATE525285T1/de

Links

Classifications

    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Body Structure For Vehicles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
AT09742260T 2008-04-10 2009-04-07 Schallbehandlungsplatte mit integrierter verbindungsverstärkung ATE525285T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0852410A FR2929991B1 (fr) 2008-04-10 2008-04-10 Panneau pour le traitement acoustique integrant un renfort de liaison
PCT/FR2009/050597 WO2009136062A2 (fr) 2008-04-10 2009-04-07 Panneau pour le traitement acoustique integrant un renfort de liaison

Publications (1)

Publication Number Publication Date
ATE525285T1 true ATE525285T1 (de) 2011-10-15

Family

ID=39929602

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09742260T ATE525285T1 (de) 2008-04-10 2009-04-07 Schallbehandlungsplatte mit integrierter verbindungsverstärkung

Country Status (10)

Country Link
US (1) US8602346B2 (de)
EP (1) EP2262686B1 (de)
JP (1) JP5459798B2 (de)
CN (1) CN101998922A (de)
AT (1) ATE525285T1 (de)
BR (1) BRPI0906895A2 (de)
CA (1) CA2719898C (de)
FR (1) FR2929991B1 (de)
RU (1) RU2494929C2 (de)
WO (1) WO2009136062A2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010086560A2 (fr) * 2009-02-02 2010-08-05 Airbus Operations Sas Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise
FR2954281B1 (fr) * 2009-12-22 2012-04-06 Airbus Operations Sas Panneau pour le traitement acoustique a epaisseur evolutive
FR2971232B1 (fr) * 2011-02-04 2013-01-18 Aircelle Sa Procede de fabrication d'une structure d'entree d'air de nacelle de turboreacteur
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
FR2975972B1 (fr) * 2011-06-01 2013-11-22 Aircelle Sa Structure d'entree d'air de nacelle de turboreacteur
FR2976556B1 (fr) * 2011-06-17 2013-12-27 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule
US20140123679A1 (en) * 2012-11-07 2014-05-08 United Technologies Corporation Flexible heat shield for a gas turbine engine
US9587563B2 (en) 2015-07-21 2017-03-07 The Boeing Company Sound attenuation apparatus and method
US9771868B2 (en) * 2015-07-21 2017-09-26 The Boeing Company Sound attenuation apparatus and method
CN105089800A (zh) * 2015-08-26 2015-11-25 成都博世德能源科技股份有限公司 一种降噪型燃气轮机进气系统
FR3060651B1 (fr) * 2016-12-20 2020-11-06 Airbus Operations Sas Structure d'entree d'air pour une nacelle d'aeronef

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4441578A (en) * 1981-02-02 1984-04-10 Rohr Industries, Inc. Encapsulated bulk absorber acoustic treatments for aircraft engine application
FR2787509B1 (fr) * 1998-12-21 2001-03-30 Aerospatiale Structure d'entree d'air pour moteur d'aeronef
US6227492B1 (en) * 1999-08-06 2001-05-08 Bell Helicopter Textron Inc. Redundant ice management system for aircraft
US6688558B2 (en) * 1999-11-23 2004-02-10 The Boeing Company Method and apparatus for aircraft inlet ice protection
GB2388184A (en) * 2002-05-03 2003-11-05 Gibbs Int Tech Ltd Amphibious vehicle dual engine cooling system
JP2004240224A (ja) * 2003-02-06 2004-08-26 Ishikawajima Harima Heavy Ind Co Ltd 吸音板固定構造
RU2267628C1 (ru) * 2004-03-25 2006-01-10 Открытое акционерное общество "Авиадвигатель" Звукопоглощающая панель для тракта турбовентиляторного двигателя
FR2887519B1 (fr) * 2005-06-22 2008-10-10 Airbus France Sas Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif

Also Published As

Publication number Publication date
EP2262686B1 (de) 2011-09-21
EP2262686A2 (de) 2010-12-22
US8602346B2 (en) 2013-12-10
FR2929991B1 (fr) 2010-05-07
WO2009136062A2 (fr) 2009-11-12
CN101998922A (zh) 2011-03-30
JP2011516786A (ja) 2011-05-26
JP5459798B2 (ja) 2014-04-02
CA2719898A1 (fr) 2009-11-12
WO2009136062A3 (fr) 2009-12-30
RU2010145546A (ru) 2012-05-20
FR2929991A1 (fr) 2009-10-16
BRPI0906895A2 (pt) 2015-07-21
RU2494929C2 (ru) 2013-10-10
US20110114787A1 (en) 2011-05-19
CA2719898C (fr) 2016-06-14

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Legal Events

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