CN101952168B - 一种特别适于飞行器发动机舱进气道的消音处理结构 - Google Patents

一种特别适于飞行器发动机舱进气道的消音处理结构 Download PDF

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Publication number
CN101952168B
CN101952168B CN2008801230323A CN200880123032A CN101952168B CN 101952168 B CN101952168 B CN 101952168B CN 2008801230323 A CN2008801230323 A CN 2008801230323A CN 200880123032 A CN200880123032 A CN 200880123032A CN 101952168 B CN101952168 B CN 101952168B
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China
Prior art keywords
sound
substructure
support portion
resistance
acoustic processing
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CN2008801230323A
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Chinese (zh)
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CN101952168A (zh
Inventor
阿兰·波特
雅克·拉兰纳
法布里斯·冈蒂耶
雅克·巴里约-克勒泽
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Airbus Operations SAS
Creuzet Aeronautique
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Airbus Operations SAS
Creuzet Aeronautique
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    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • 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
    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN2008801230323A 2007-12-21 2008-12-16 一种特别适于飞行器发动机舱进气道的消音处理结构 Active CN101952168B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0760194A FR2925463B1 (fr) 2007-12-21 2007-12-21 Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef
FR0760194 2007-12-21
PCT/FR2008/052312 WO2009081020A1 (fr) 2007-12-21 2008-12-16 Structure pour le traitement acoustique plus particulierement adaptee a une entree d'air d'une nacelle d'aeronef

Publications (2)

Publication Number Publication Date
CN101952168A CN101952168A (zh) 2011-01-19
CN101952168B true CN101952168B (zh) 2013-12-11

Family

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Application Number Title Priority Date Filing Date
CN2008801230323A Active CN101952168B (zh) 2007-12-21 2008-12-16 一种特别适于飞行器发动机舱进气道的消音处理结构

Country Status (9)

Country Link
US (1) US8413922B2 (https=)
EP (1) EP2244939B1 (https=)
JP (1) JP2011506852A (https=)
CN (1) CN101952168B (https=)
BR (1) BRPI0819482A2 (https=)
CA (1) CA2709331C (https=)
FR (1) FR2925463B1 (https=)
RU (1) RU2482020C2 (https=)
WO (1) WO2009081020A1 (https=)

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FR2950325B1 (fr) * 2009-09-23 2011-09-09 Airbus Operations Sas Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef
FR2953811B1 (fr) * 2009-12-15 2012-03-16 Airbus Operations Sas Panneau pour une entree d'air d'une nacelle d'aeronef assurant un traitement acoustique et un traitement du givre optimises
DE102011008920A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Schallabsorber, insbesondere für einen Gasturbinenabgaskonus und Verfahren zu dessen Herstellung
FR2976557B1 (fr) * 2011-06-20 2013-07-12 Airbus Operations Sas Procede de realisation d'un panneau pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
FR2980774B1 (fr) * 2011-10-03 2013-10-25 Airbus Operations Sas Nacelle d'aeronef comportant un dispositif d'alimentation en air chaud d'un panneau combinant les traitements acoustique et du givre
FR2980776B1 (fr) * 2011-10-03 2014-08-22 Airbus Operations Sas Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins un canal annulaire
FR2981049B1 (fr) * 2011-10-07 2014-04-11 Aircelle Sa Procede de fabrication d'un panneau d'absorption acoustique
US9488067B2 (en) * 2014-01-14 2016-11-08 The Boeing Company Aircraft anti-icing systems having deflector vanes
US9592918B2 (en) 2014-06-23 2017-03-14 Rohr, Inc. Acoustic liner
US9771868B2 (en) * 2015-07-21 2017-09-26 The Boeing Company Sound attenuation apparatus and method
US9587563B2 (en) 2015-07-21 2017-03-07 The Boeing Company Sound attenuation apparatus and method
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
US9764818B2 (en) 2016-02-10 2017-09-19 Rohr, Inc. Structural, cellular core with corrugated support walls
US9761216B2 (en) 2016-02-10 2017-09-12 Rohr, Inc. Acoustic panel with angled corrugated core structures
US9704467B1 (en) 2016-04-15 2017-07-11 Rohr, Inc. Acoustic panel with corrugated baffles and septums
US9978354B2 (en) * 2016-04-15 2018-05-22 Rohr, Inc. Acoustic panel with vertical stiffeners
FR3060829B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Structure constituant un isolant acoustique
US10414481B2 (en) 2017-02-14 2019-09-17 Rohr, Inc. Method for forming a structural panel
US10525636B2 (en) 2017-06-19 2020-01-07 Rohr, Inc. Process for forming a fiber-reinforced composite structure
US10695986B2 (en) 2017-08-22 2020-06-30 Rohr, Inc. Method for forming a structural panel
FR3070674B1 (fr) 2017-09-06 2019-09-13 Safran Nacelles Integration a la levre acoustique degivree
US11125157B2 (en) * 2017-09-22 2021-09-21 The Boeing Company Advanced inlet design
FR3074776B1 (fr) 2017-12-13 2020-02-28 Safran Nacelles Levre d’entree d’air de nacelle pour turboreacteur
FR3077800B1 (fr) * 2018-02-12 2020-09-25 Safran Nacelles Dispositif de degivrage et de traitement acoustique pour une levre d’entree d’air d’une nacelle de turboreacteur
US10906659B2 (en) 2018-04-03 2021-02-02 Rohr, Inc. Structured panel with structural reinforcement(s)
FR3083265A1 (fr) 2018-06-29 2020-01-03 Airbus Operations Structure d'entree d'air pour une nacelle d'aeronef comportant un element amortisseur de chocs
US11396366B2 (en) 2018-09-28 2022-07-26 Rohr, Inc. Active laminar flow control structural plenums fastened
US11524770B2 (en) * 2018-09-28 2022-12-13 Rohr, Inc. Active laminar flow control plenum panel arrangements and installation methods
US11414203B2 (en) 2018-09-28 2022-08-16 Rohr, Inc. Active laminar flow control plenum panel arrangement
US11398214B2 (en) 2018-12-14 2022-07-26 Rohr, Inc. Forming a structured panel with one or more structural reinforcements
US11242822B2 (en) 2018-12-14 2022-02-08 Rohr, Inc. Structured panel with multi-panel structure(s)
US11572850B2 (en) 2019-06-04 2023-02-07 Rohr, Inc. Acoustic panel with one or more structural stiffeners
FR3100842A1 (fr) * 2019-09-12 2021-03-19 Airbus Operations Entrée d'air, nacelle, ensemble propulsif et aéronef à lèvre rainurée

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EP1398473A1 (fr) * 2002-09-10 2004-03-17 Airbus France Couche acoustiquement resistive pour panneau d'atténuation acoustique, panneau utilisant une telle couche

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EP1232945A1 (fr) * 2001-02-15 2002-08-21 AIRBUS FRANCE (Société par Actions Simplifiée) Procédé de dégivrage d'un capot d'entrée d'air de moteur à réaction et dispositif pour sa mise en oeuvre
EP1398473A1 (fr) * 2002-09-10 2004-03-17 Airbus France Couche acoustiquement resistive pour panneau d'atténuation acoustique, panneau utilisant une telle couche

Also Published As

Publication number Publication date
JP2011506852A (ja) 2011-03-03
US20100276548A1 (en) 2010-11-04
RU2010130454A (ru) 2012-01-27
WO2009081020A1 (fr) 2009-07-02
FR2925463B1 (fr) 2010-04-23
BRPI0819482A2 (pt) 2015-05-05
CN101952168A (zh) 2011-01-19
RU2482020C2 (ru) 2013-05-20
CA2709331C (fr) 2016-06-07
EP2244939B1 (fr) 2013-03-20
CA2709331A1 (fr) 2009-07-02
US8413922B2 (en) 2013-04-09
FR2925463A1 (fr) 2009-06-26
EP2244939A1 (fr) 2010-11-03

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