BRPI0914577A2 - painel acústico para bocal exaustor, bocal exaustor para nacela e nacela - Google Patents
painel acústico para bocal exaustor, bocal exaustor para nacela e nacelaInfo
- Publication number
- BRPI0914577A2 BRPI0914577A2 BRPI0914577A BRPI0914577A BRPI0914577A2 BR PI0914577 A2 BRPI0914577 A2 BR PI0914577A2 BR PI0914577 A BRPI0914577 A BR PI0914577A BR PI0914577 A BRPI0914577 A BR PI0914577A BR PI0914577 A2 BRPI0914577 A2 BR PI0914577A2
- Authority
- BR
- Brazil
- Prior art keywords
- nacelle
- exhaust nozzle
- acoustic panel
- exhaust
- nozzle
- Prior art date
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
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
-
- 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
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D33/06—Silencing exhaust or propulsion jets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/501—Elasticity
-
- 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)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Golf Clubs (AREA)
- Connection Of Plates (AREA)
- Exhaust Silencers (AREA)
- Laminated Bodies (AREA)
- Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0803559A FR2933224B1 (fr) | 2008-06-25 | 2008-06-25 | Panneau accoustique pour une tuyere d'ejection |
PCT/FR2009/050900 WO2010007263A1 (fr) | 2008-06-25 | 2009-05-14 | Panneau acoustique pour une tuyère d'éjection |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0914577A2 true BRPI0914577A2 (pt) | 2015-12-15 |
Family
ID=40325898
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0914577A BRPI0914577A2 (pt) | 2008-06-25 | 2009-05-14 | painel acústico para bocal exaustor, bocal exaustor para nacela e nacela |
Country Status (9)
Country | Link |
---|---|
US (1) | US8640825B2 (pt) |
EP (1) | EP2291840B1 (pt) |
CN (1) | CN102067207A (pt) |
BR (1) | BRPI0914577A2 (pt) |
CA (1) | CA2726463A1 (pt) |
ES (1) | ES2566759T3 (pt) |
FR (1) | FR2933224B1 (pt) |
RU (1) | RU2526215C2 (pt) |
WO (1) | WO2010007263A1 (pt) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120308379A1 (en) * | 2011-05-31 | 2012-12-06 | Mra Systems, Inc. | Aircraft engine cowl and process therefor |
US9514734B1 (en) | 2011-06-30 | 2016-12-06 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Acoustic liners for turbine engines |
FR2980902B1 (fr) | 2011-10-04 | 2013-09-13 | Aircelle Sa | Panneau d'attenuation acoustique structural |
US8944753B2 (en) | 2011-11-09 | 2015-02-03 | Pratt & Whitney Canada Corp. | Strut mounting arrangement for gas turbine exhaust case |
US8826669B2 (en) | 2011-11-09 | 2014-09-09 | Pratt & Whitney Canada Corp. | Gas turbine exhaust case |
US9200537B2 (en) * | 2011-11-09 | 2015-12-01 | Pratt & Whitney Canada Corp. | Gas turbine exhaust case with acoustic panels |
US10837367B2 (en) * | 2012-02-28 | 2020-11-17 | Raytheon Technologies Corporation | Acoustic treatment in an unducted area of a geared turbomachine |
US9856745B2 (en) * | 2012-02-28 | 2018-01-02 | United Technologies Corporation | Acoustic treatment in an unducted area of a geared turbomachine |
FR2989814B1 (fr) * | 2012-04-20 | 2015-05-01 | Aircelle Sa | Panneau mince d'absorption d'ondes acoustiques emises par un turboreacteur de nacelle d'aeronef, et nacelle equipee d'un tel panneau |
US8651233B2 (en) * | 2012-05-08 | 2014-02-18 | Hexcel Corporation | Acoustic structure with increased bandwidth suppression |
FR2994115B1 (fr) | 2012-08-02 | 2015-02-20 | Aircelle Sa | Ensemble d'outillage pour la fabrication d'une piece metallique de revolution et procede de fabrication d'une telle piece |
FR2995360B1 (fr) * | 2012-09-12 | 2018-06-15 | Snecma | Procede de montage d'un panneau acoustique dans un carter d'une turbomachine et turbomachine comportant un panneau acoustique |
EP2961967B1 (en) | 2013-03-01 | 2021-03-31 | Raytheon Technologies Corporation | Repair of surface damage at edges of cellular panels |
FR3013076B1 (fr) * | 2013-11-13 | 2017-12-08 | Ge Energy Products France Snc | Structure de protection thermo-acoustique pour machine tournante |
FR3013629B1 (fr) * | 2013-11-26 | 2016-07-29 | Eurocopter France | Panneau d'habillage insonorisant et aeronef |
US9352529B2 (en) * | 2014-08-12 | 2016-05-31 | Hrl Laboratories, Llc | Progressive stiffness structural-acoustic sandwich panel |
FR3036061B1 (fr) * | 2015-05-12 | 2019-08-16 | Safran Nacelles | Panneau composite et nacelle de turboreacteur d’aeronef comprenant un tel panneau |
FR3039147B1 (fr) * | 2015-07-24 | 2017-08-25 | Aircelle Sa | Panneau d’attenuation acoustique en materiau composite ceramique oxyde avec ame en materiau metallique converti electrochimiquement |
FR3032966A1 (fr) * | 2015-07-24 | 2016-08-26 | Aircelle Sa | Panneau d’attenuation acoustique en materiau composite a matrice ceramique et a ame metallique |
FR3044961B1 (fr) * | 2015-12-15 | 2018-01-19 | Safran Nacelles | Panneau pour nacelle de turboreacteur comportant une protection thermique et procede de fabrication d’un tel panneau |
US10156207B2 (en) * | 2016-01-05 | 2018-12-18 | Medhat Osman | Ultra hush exhaust system (UHES) |
FR3058672B1 (fr) * | 2016-11-14 | 2019-05-10 | Safran | Volet inverseur de poussee, et procede de fabrication |
US10247021B2 (en) | 2016-12-07 | 2019-04-02 | Rohr, Inc. | High temperature seals for blanketless inner fixed structure |
FR3070438B1 (fr) * | 2017-08-25 | 2020-09-11 | Safran Nacelles | Structure alveolaire et dispositif d’attenuation acoustique pour nacelle d'ensemble propulsif d'aeronef |
US10677163B2 (en) * | 2017-12-06 | 2020-06-09 | General Electric Company | Noise attenuation structures |
US11092077B2 (en) * | 2018-03-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Aircraft component and method of manufacture |
FR3081510B1 (fr) | 2018-05-24 | 2020-05-29 | Safran Nacelles | Panneau d’attenuation acoustique pour nacelle de turboreacteur d’aeronef |
FR3084917B1 (fr) * | 2018-08-09 | 2021-04-16 | Safran Ceram | Ensemble pour une tuyere d'ejection de turbomachine |
US11353240B2 (en) | 2018-10-02 | 2022-06-07 | United States Of America As Represented By The Administrator Of Nasa | Low drag, variable-depth acoustic liner |
FR3088905A1 (fr) * | 2018-11-28 | 2020-05-29 | Airbus Operations (S.A.S.) | Structure d’absorption acoustique comprenant un système de drainage de liquide et ensemble propulsif comportant une telle structure d’absorption acoustique |
FR3093025B1 (fr) * | 2019-02-26 | 2023-03-24 | Safran Nacelles | Système alvéolaire dilatable pour panneau sandwich |
GB201903262D0 (en) * | 2019-03-11 | 2019-04-24 | Rolls Royce Plc | Efficient gas turbine engine installation and operation |
RU2720151C1 (ru) * | 2019-04-23 | 2020-04-24 | федеральное государственное бюджетное образовательное учреждение высшего образования "Пермский национальный исследовательский политехнический университет" | Способ изготовления звукопоглощающей конструкции |
FR3095674B1 (fr) * | 2019-05-03 | 2021-04-16 | Safran Aircraft Engines | Grille d’inverseur de poussée incluant un traitement acoustique |
GB2583751B (en) * | 2019-05-09 | 2022-02-02 | Safran Nacelles Ltd | Acoustic panel |
US11028732B2 (en) | 2019-09-05 | 2021-06-08 | Rolls-Royce North American Technologies Inc. | High temperature panel damper for sheet metal structures |
FR3106334B1 (fr) * | 2020-01-20 | 2024-04-05 | Airbus Operations Sas | Panneau isolant multicouche à renforts de fixation intégrés et procédé de fabrication d’un tel panneau |
FR3111949B1 (fr) * | 2020-06-26 | 2022-06-10 | Safran Ceram | Caisson acoustique pour un cône d’éjection |
US11867077B2 (en) | 2021-06-07 | 2024-01-09 | Rohr, Inc. | Acoustic structure with floating interior skin |
US11732673B2 (en) * | 2021-07-27 | 2023-08-22 | General Electric Company | Variable area exhaust nozzle system and method for control thereof |
US11635026B1 (en) * | 2021-12-21 | 2023-04-25 | Rolls-Royce Deutschland Ltd & Co Kg | Fan case assembly for a gas turbine engine |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3630312A (en) * | 1969-11-07 | 1971-12-28 | Rohr Corp | Sound absorptive honeycomb sandwich panel with multilayer, porous, structural facing |
US3819007A (en) * | 1973-04-27 | 1974-06-25 | Lockheed Aircraft Corp | Controllable laminar sound absorptive structure |
US3977146A (en) * | 1974-12-18 | 1976-08-31 | Standard Pressed Steel Co. | Fastener bushing |
US4465725A (en) * | 1982-07-15 | 1984-08-14 | Rohr Industries, Inc. | Noise suppression panel |
US5594216A (en) * | 1994-11-29 | 1997-01-14 | Lockheed Missiles & Space Co., Inc. | Jet engine sound-insulation structure |
US6009789A (en) * | 1997-05-01 | 2000-01-04 | Simula Inc. | Ceramic tile armor with enhanced joint and edge protection |
EP0895223B1 (en) * | 1997-07-30 | 2003-04-16 | The Boeing Company | Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring |
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 |
US20010048048A1 (en) * | 1999-01-13 | 2001-12-06 | Brian L Riedel | Backside fitting attachment for nacelle acoustic panels |
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 |
GB0016149D0 (en) * | 2000-06-30 | 2000-08-23 | Short Brothers Plc | A noise attenuation panel |
US6509081B1 (en) * | 2000-09-28 | 2003-01-21 | The Boeing Company | No-septum acoustic sandwich panel, and apparatus and method for suppressing noise in a nozzle |
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 |
RU2230208C2 (ru) * | 2002-06-05 | 2004-06-10 | Открытое акционерное общество "Авиадвигатель" | Устройство для звукопоглощения в двухконтурном турбореактивном двигателе |
FR2840647B1 (fr) * | 2002-06-05 | 2004-10-29 | Airbus France | Dispositif pour le raccordement de deux pieces tubulaires de turboreacteur d'aeronef |
JP2004027788A (ja) * | 2002-06-21 | 2004-01-29 | Junsei:Kk | 発泡体充填ハニカム材層に空気空間を持つ吸音パネル構造体 |
FR2850410B1 (fr) * | 2003-01-24 | 2006-02-03 | Hutchinson | Panneau d'isolation acoustique |
US6868940B1 (en) * | 2003-04-29 | 2005-03-22 | Julius Mekwinski | Sound absorbing panel |
US7565950B2 (en) * | 2005-01-26 | 2009-07-28 | The Aerospace Corporation | Sound suppression material and method |
-
2008
- 2008-06-25 FR FR0803559A patent/FR2933224B1/fr not_active Expired - Fee Related
-
2009
- 2009-05-14 WO PCT/FR2009/050900 patent/WO2010007263A1/fr active Application Filing
- 2009-05-14 CA CA2726463A patent/CA2726463A1/fr not_active Abandoned
- 2009-05-14 EP EP09784386.6A patent/EP2291840B1/fr active Active
- 2009-05-14 RU RU2011100140/28A patent/RU2526215C2/ru not_active IP Right Cessation
- 2009-05-14 US US13/000,720 patent/US8640825B2/en active Active
- 2009-05-14 ES ES09784386.6T patent/ES2566759T3/es active Active
- 2009-05-14 BR BRPI0914577A patent/BRPI0914577A2/pt not_active IP Right Cessation
- 2009-05-14 CN CN2009801234723A patent/CN102067207A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
RU2011100140A (ru) | 2012-07-27 |
US8640825B2 (en) | 2014-02-04 |
FR2933224B1 (fr) | 2010-10-29 |
RU2526215C2 (ru) | 2014-08-20 |
WO2010007263A1 (fr) | 2010-01-21 |
ES2566759T3 (es) | 2016-04-15 |
EP2291840A1 (fr) | 2011-03-09 |
US20110108357A1 (en) | 2011-05-12 |
FR2933224A1 (fr) | 2010-01-01 |
CA2726463A1 (fr) | 2010-01-21 |
EP2291840B1 (fr) | 2016-01-13 |
CN102067207A (zh) | 2011-05-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25A | Requested transfer of rights approved |
Owner name: AIRCELLE (FR) , SME (FR) |
|
B25D | Requested change of name of applicant approved |
Owner name: AIRCELLE (FR) , HERAKLES (FR) |
|
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] |