BR112014008180A2 - método de fabricação de um painel de absorção de som, painel de absorção de som e nacela - Google Patents

método de fabricação de um painel de absorção de som, painel de absorção de som e nacela

Info

Publication number
BR112014008180A2
BR112014008180A2 BR112014008180A BR112014008180A BR112014008180A2 BR 112014008180 A2 BR112014008180 A2 BR 112014008180A2 BR 112014008180 A BR112014008180 A BR 112014008180A BR 112014008180 A BR112014008180 A BR 112014008180A BR 112014008180 A2 BR112014008180 A2 BR 112014008180A2
Authority
BR
Brazil
Prior art keywords
sound
absorbing panel
nacelle
manufacturing
absorbing
Prior art date
Application number
BR112014008180A
Other languages
English (en)
Inventor
Hurlin Hervé
Caruel Pierre
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
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112014008180A2 publication Critical patent/BR112014008180A2/pt

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
    • G10K11/18—Methods or devices for transmitting, conducting or directing sound
    • G10K11/20—Reflecting arrangements
    • 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
    • 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
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • 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
    • 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
    • B64D2033/0233—Arrangements 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Exhaust Silencers (AREA)
  • Building Environments (AREA)
BR112014008180A 2011-10-07 2012-10-03 método de fabricação de um painel de absorção de som, painel de absorção de som e nacela BR112014008180A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1159059A FR2981049B1 (fr) 2011-10-07 2011-10-07 Procede de fabrication d'un panneau d'absorption acoustique
PCT/FR2012/052232 WO2013050698A1 (fr) 2011-10-07 2012-10-03 Procédé de fabrication d'un panneau d'absorption acoustique

Publications (1)

Publication Number Publication Date
BR112014008180A2 true BR112014008180A2 (pt) 2017-04-18

Family

ID=47071397

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014008180A BR112014008180A2 (pt) 2011-10-07 2012-10-03 método de fabricação de um painel de absorção de som, painel de absorção de som e nacela

Country Status (8)

Country Link
US (1) US9390704B2 (pt)
EP (1) EP2763892B1 (pt)
CN (1) CN104024104A (pt)
BR (1) BR112014008180A2 (pt)
CA (1) CA2850455A1 (pt)
FR (1) FR2981049B1 (pt)
RU (1) RU2014117394A (pt)
WO (1) WO2013050698A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3013329B1 (fr) 2013-11-15 2017-08-11 Aircelle Sa Dispositif de degivrage d’entree d’air de nacelle d’un moteur d’aeronef, procede de fabrication d’un tel dispositif de degivrage et nacelle de moteur d’aeronef equipe d’un tel dispositif de degivrage
EP3038101B1 (fr) * 2014-12-23 2022-11-23 Airbus (Sas) Paroi acoustique à échangeur thermique intégré
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
CN106042503B (zh) * 2016-05-31 2018-03-09 航天材料及工艺研究所 一种超轻质夹层结构复合材料的制备方法
FR3070674B1 (fr) 2017-09-06 2019-09-13 Safran Nacelles Integration a la levre acoustique degivree
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
CA184858S (en) * 2018-05-28 2019-11-29 Trenkle & Trenkle Gbr Acupressure mat
FR3085437B1 (fr) * 2018-09-05 2020-11-20 Airbus Operations Sas Structure d’entree d’air d’une nacelle d’aeronef
FR3087419B1 (fr) * 2018-10-19 2020-10-30 Airbus Operations Sas Nacelle de moteur d’aeronef comprenant un systeme de protection contre le givre.
DE102019111135A1 (de) * 2019-04-30 2020-11-05 Airbus Operations Gmbh Vorderkantenvorrichtung für ein Flugzeug
FR3130754B1 (fr) 2021-12-17 2024-05-10 Safran Nacelles Levre d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB802686A (en) * 1955-03-31 1958-10-08 Bettinger Corp Improvements in or relating to honeycomb structures
US2980573A (en) * 1959-05-07 1961-04-18 Union Bag Camp Paper Corp Ventilated honeycomb
US3933327A (en) 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
US4094717A (en) * 1975-06-03 1978-06-13 Aai Corporation Method of assembly of an insulating panel arrangement
US4001473A (en) * 1976-02-19 1977-01-04 Rohr Industries, Inc. Sound attenuating structural honeycomb sandwich material
US4752049A (en) * 1985-12-30 1988-06-21 The Boeing Company Leading edge slat/anti-icing system and method for airfoil
US4957577A (en) * 1988-04-04 1990-09-18 Plascore, Inc. Method for making welded honeycomb core
GB8817669D0 (en) * 1988-07-25 1988-09-01 Short Brothers Ltd Means for attenuating sound energy
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
WO1993001048A1 (en) * 1991-07-12 1993-01-21 Hexcel Corporation Method and apparatus for making thermally fused thermoplastic honeycomb structures
US5337978A (en) * 1992-10-29 1994-08-16 The B.F. Goodrich Company Leading edge pneumatic deicer assembly
US5841079A (en) 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
US6245407B1 (en) * 1999-04-27 2001-06-12 Hexcel Corporation Thermoformable honeycomb structures
US6371411B1 (en) 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
US6688558B2 (en) * 1999-11-23 2004-02-10 The Boeing Company Method and apparatus for aircraft inlet ice protection
FR2820715B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR2820716B1 (fr) * 2001-02-15 2003-05-30 Eads Airbus Sa Procede de degivrage par circulation forcee d'un fluide, d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
DE102004024007B4 (de) * 2004-05-13 2007-10-11 Airbus Deutschland Gmbh Flugzeugkomponente, insbesondere Flügel
WO2007149535A1 (en) * 2006-06-21 2007-12-27 Ben Strauss Honeycomb with a fraction of substantially porous cell walls
FR2904604B1 (fr) * 2006-08-04 2009-02-27 Airbus France Sas Element de structure d'un aeronef
EP2140120A2 (fr) * 2007-02-20 2010-01-06 AIRBUS France Procede de realisation d'un revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe et revetement pour le traitement acoustique ainsi obtenu
FR2912781B1 (fr) * 2007-02-20 2009-04-10 Airbus France Sas Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
FR2917067B1 (fr) * 2007-06-08 2009-08-21 Airbus France Sas Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
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
US8215585B2 (en) * 2008-05-13 2012-07-10 The Boeing Company Impact resistant core
FR2934566B1 (fr) * 2008-08-04 2011-03-11 Aircelle Sa Procede de fabrication d'un ensemble de degivrage sur un panneau d'une nacelle.
WO2010089496A1 (fr) * 2009-02-03 2010-08-12 Airbus Operations Sas Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef
WO2010119946A1 (ja) * 2009-04-16 2010-10-21 岐阜プラスチック工業 株式会社 構造体及び成形品並びにそれらの製造方法
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
FR2976709B1 (fr) * 2011-06-20 2013-07-12 Airbus Operations Sas Procede de realisation d'un panneau pour le traitement acoustique integrant des canaux juxtaposes a une structure alveolaire
FR2983835B1 (fr) * 2011-12-13 2014-02-21 Airbus Operations Sas Procede de realisation d'un panneau pour le traitement acoustique

Also Published As

Publication number Publication date
US20140216846A1 (en) 2014-08-07
FR2981049A1 (fr) 2013-04-12
RU2014117394A (ru) 2015-11-20
EP2763892B1 (fr) 2018-01-24
CN104024104A (zh) 2014-09-03
US9390704B2 (en) 2016-07-12
CA2850455A1 (fr) 2013-04-11
FR2981049B1 (fr) 2014-04-11
WO2013050698A1 (fr) 2013-04-11
EP2763892A1 (fr) 2014-08-13

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]