BRPI0918600A2 - método para fazer painel acústico de uma aba de entrada de ar de uma nacela, aba de entrada de ar compreendendo painel, nacela de motor turboeixo - Google Patents

método para fazer painel acústico de uma aba de entrada de ar de uma nacela, aba de entrada de ar compreendendo painel, nacela de motor turboeixo

Info

Publication number
BRPI0918600A2
BRPI0918600A2 BRPI0918600A BRPI0918600A BRPI0918600A2 BR PI0918600 A2 BRPI0918600 A2 BR PI0918600A2 BR PI0918600 A BRPI0918600 A BR PI0918600A BR PI0918600 A BRPI0918600 A BR PI0918600A BR PI0918600 A2 BRPI0918600 A2 BR PI0918600A2
Authority
BR
Brazil
Prior art keywords
air intake
panel
intake flap
nacelle
turbocharger engine
Prior art date
Application number
BRPI0918600A
Other languages
English (en)
Inventor
Pierre Caruel
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 BRPI0918600A2 publication Critical patent/BRPI0918600A2/pt

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
    • 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
    • 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
    • F02C7/047—Heating to prevent icing
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • H05B3/22—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible
    • H05B3/26—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor mounted on insulating base
    • H05B3/267—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor mounted on insulating base the insulating base being an organic material, e.g. plastic
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • H05B3/22—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible
    • H05B3/28—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor embedded in insulating material
    • H05B3/286—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor embedded in insulating material the insulating material being an organic material, e.g. plastic
    • 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
    • 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
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
BRPI0918600A 2008-09-03 2009-08-14 método para fazer painel acústico de uma aba de entrada de ar de uma nacela, aba de entrada de ar compreendendo painel, nacela de motor turboeixo BRPI0918600A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0804823A FR2935356B1 (fr) 2008-09-03 2008-09-03 Procede de fabrication d'un panneau acoustique d'une levre d'entree d'air d'une nacelle
PCT/FR2009/001009 WO2010026305A1 (fr) 2008-09-03 2009-08-14 Procédé de fabrication d'un panneau acoustique d'une lèvre d'entrée d'air d'une nacelle

Publications (1)

Publication Number Publication Date
BRPI0918600A2 true BRPI0918600A2 (pt) 2015-12-15

Family

ID=40488393

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0918600A BRPI0918600A2 (pt) 2008-09-03 2009-08-14 método para fazer painel acústico de uma aba de entrada de ar de uma nacela, aba de entrada de ar compreendendo painel, nacela de motor turboeixo

Country Status (9)

Country Link
US (1) US8584363B2 (pt)
EP (1) EP2321179B1 (pt)
CN (1) CN102143889B (pt)
BR (1) BRPI0918600A2 (pt)
CA (1) CA2733701A1 (pt)
ES (1) ES2457531T3 (pt)
FR (1) FR2935356B1 (pt)
RU (1) RU2500580C2 (pt)
WO (1) WO2010026305A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935357B1 (fr) * 2008-09-03 2010-08-27 Aircelle Sa Procede de fabrication d'un element de nacelle
FR2980775B1 (fr) * 2011-10-03 2014-07-11 Airbus Operations Sas Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins une chambre de stabilisation
US8998144B2 (en) * 2012-02-06 2015-04-07 Textron Innovations Inc. Thermal insulation barrier for an aircraft de-icing heater
FR2992291B1 (fr) * 2012-06-25 2016-03-04 Aircelle Sa Ensemble electrique chauffant pour dispositif de degivrage
US8919494B2 (en) * 2012-07-31 2014-12-30 Rohr, Inc. Electric heater for integration into an aircraft acoustic panel
JP2014050864A (ja) * 2012-09-07 2014-03-20 Dainippon Printing Co Ltd ラベル用レーザ加工機
ITTO20121152A1 (it) * 2012-12-27 2014-06-28 Alenia Aermacchi Spa Gondola motore per un aeromobile, dotata di un sistema integrato di protezione antighiaccio ed assorbimento acustico.
CN107108014B (zh) * 2014-12-18 2020-03-31 庞巴迪公司 用于机身部件的吸声器
FR3061132B1 (fr) * 2016-12-27 2023-11-03 Airbus Operations Sas Structure pour ensemble propulsif d'aeronef, systeme et ensemble propulsif associes
FR3079818A1 (fr) * 2018-04-10 2019-10-11 Airbus Operations (S.A.S.) Nacelle de moteur d'aeronef munie d'un systeme de protection contre le givre et procede de protection associe
CN109050869A (zh) * 2018-07-17 2018-12-21 中国航空工业集团公司沈阳飞机设计研究所 一种冲压空气引气结构
FR3086786B1 (fr) * 2018-10-01 2020-12-18 Airbus Operations Sas Procede de fabrication d'une peau acoustique degivrante pour panneau acoustique d'aeronef, utilisant un dispositif d'ecartement de fibres
FR3092871B1 (fr) * 2019-02-15 2022-02-25 Airbus Operations Sas Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef
FR3100842A1 (fr) * 2019-09-12 2021-03-19 Airbus Operations Entrée d'air, nacelle, ensemble propulsif et aéronef à lèvre rainurée
FR3115829B1 (fr) * 2020-11-05 2022-10-14 Safran Nacelles Fixation d’un cône d’éjection dans une tuyère de turbomachine
CN114162336B (zh) * 2021-12-14 2024-01-05 北京机电工程研究所 一种飞行器雷达隐身进气道及其制备方法
FR3130754B1 (fr) * 2021-12-17 2024-05-10 Safran Nacelles Levre d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef
CN114162331B (zh) * 2022-02-14 2022-04-29 中国空气动力研究与发展中心低速空气动力研究所 一种结冰探测装置及结冰探测方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB885131A (en) * 1958-04-24 1961-12-20 Goodrich Co B F Apparatus for and method of making a heating structure
ATA331285A (de) * 1985-11-13 1988-11-15 Ims Ionen Mikrofab Syst Verfahren zur herstellung einer transmissionsmaske
FR2733871B1 (fr) * 1995-05-04 1997-06-06 Norton Pampus Gmbh Element chauffant, procede de fabrication et application
GB9613615D0 (en) * 1996-06-28 1996-08-28 Short Brothers Plc Method of manufacturing a noise attenuation panel
US6371411B1 (en) * 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
RU2226481C2 (ru) * 2002-07-19 2004-04-10 Открытое акционерное общество "Казанский вертолётный завод" Электротепловая противообледенительная система, например, для лопастей вертолёта
US7588212B2 (en) * 2003-07-08 2009-09-15 Rohr Inc. Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
US7824824B2 (en) * 2005-03-08 2010-11-02 Texas Instruments Incorporated Composite phase shifting lithography mask including etch stop layer
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
DE102006031330B4 (de) * 2005-07-14 2014-03-20 Goodrich Corp. Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung
US7923668B2 (en) * 2006-02-24 2011-04-12 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US7291815B2 (en) * 2006-02-24 2007-11-06 Goodrich Corporation Composite ice protection heater and method of producing same
FR2908737B1 (fr) * 2006-11-16 2009-12-04 Airbus France Revetement acoustique pour aeronef incorporant un systeme de traitement du givre par effet joule.
DE102009000642B4 (de) * 2009-02-05 2012-12-06 BAM Bundesanstalt für Materialforschung und -prüfung Verfahren zur Herstellung mikrostrukturierter Bauteile mittels Photolithographie

Also Published As

Publication number Publication date
FR2935356A1 (fr) 2010-03-05
ES2457531T3 (es) 2014-04-28
CA2733701A1 (fr) 2010-03-11
RU2011111341A (ru) 2012-10-10
FR2935356B1 (fr) 2010-08-27
CN102143889A (zh) 2011-08-03
WO2010026305A1 (fr) 2010-03-11
CN102143889B (zh) 2013-12-25
RU2500580C2 (ru) 2013-12-10
EP2321179B1 (fr) 2014-01-15
US8584363B2 (en) 2013-11-19
US20110155855A1 (en) 2011-06-30
EP2321179A1 (fr) 2011-05-18

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2376 DE 19-07-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.