FR2356820A1 - Structure d'insonorisation, notamment pour tuyere de moteur a turbine a gaz - Google Patents

Structure d'insonorisation, notamment pour tuyere de moteur a turbine a gaz

Info

Publication number
FR2356820A1
FR2356820A1 FR7720271A FR7720271A FR2356820A1 FR 2356820 A1 FR2356820 A1 FR 2356820A1 FR 7720271 A FR7720271 A FR 7720271A FR 7720271 A FR7720271 A FR 7720271A FR 2356820 A1 FR2356820 A1 FR 2356820A1
Authority
FR
France
Prior art keywords
gas turbine
panel
turbine engine
sound insulation
insulation structure
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7720271A
Other languages
English (en)
Other versions
FR2356820B1 (fr
Inventor
Dudley Owen Nash
Joseph Holowach
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2356820A1 publication Critical patent/FR2356820A1/fr
Application granted granted Critical
Publication of FR2356820B1 publication Critical patent/FR2356820B1/fr
Granted legal-status Critical Current

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Exhaust Silencers (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Laminated Bodies (AREA)

Abstract

Structure utilisant les avantages inhérents du matériau sandwich en nid d'abeilles sans le soumettre à des niveaux élevés de contraintes thermiques. La structure comporte une paroi de conduit 18 dans laquelle un panneau acoustique basse fréquence 38 est encastré en retrait de façon à former une poche dans laquelle coulisse un panneau acoustique haute fréquence du type sandwich en nid d'abeilles 26 au moyen de joints glissants 54, le panneau basse fréquence étant également du type sandwich comportant une série de cellules munies de tubes saillants 42 qui traversent avec jeu des ouvertures 52 formées dans le panneau haute fréquence pour déboucher dans le conduit où le bruit est engendré. Application à l'insonorisation des tuyères des moteurs à turbines à gaz.
FR7720271A 1976-07-02 1977-07-01 Structure d'insonorisation, notamment pour tuyere de moteur a turbine a gaz Granted FR2356820A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/702,115 US4106587A (en) 1976-07-02 1976-07-02 Sound-suppressing structure with thermal relief

Publications (2)

Publication Number Publication Date
FR2356820A1 true FR2356820A1 (fr) 1978-01-27
FR2356820B1 FR2356820B1 (fr) 1983-05-20

Family

ID=24819921

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7720271A Granted FR2356820A1 (fr) 1976-07-02 1977-07-01 Structure d'insonorisation, notamment pour tuyere de moteur a turbine a gaz

Country Status (6)

Country Link
US (1) US4106587A (fr)
JP (1) JPS6014893B2 (fr)
DE (1) DE2729568A1 (fr)
FR (1) FR2356820A1 (fr)
GB (1) GB1520720A (fr)
IT (1) IT1083790B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2588614A1 (fr) * 1985-10-16 1987-04-17 Nuovo Pignone Spa Silencieux d'echappement pour turbine a gaz de forte puissance.
EP0219218A1 (fr) * 1985-09-05 1987-04-22 AlliedSignal Inc. Dispositif d'insonorisation
FR2685386A1 (fr) * 1991-12-20 1993-06-25 Europ Propulsion Systeme d'amortissement des instabilites de combustion haute frequence dans une chambre de combustion.
EP1849974A2 (fr) * 2006-04-27 2007-10-31 United Technologies Corporation Résonateur de pointe arrière pour moteur de turbine
DE102015117092A1 (de) 2013-11-13 2016-04-21 Ge Energy Products France Snc Thermoakustische Schutzstruktur für eine rotierende Maschine
FR3065754A1 (fr) * 2017-04-28 2018-11-02 Safran Aircraft Engines Cellule d'absorption acoustique pour turboreacteur et panneau de traitement acoustique associe

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DK142710B (da) * 1977-11-10 1980-12-29 Elektronikcentralen Lydabsorberende struktur.
DE2853613C2 (de) * 1977-12-22 1984-08-16 Rolls-Royce Ltd., London Schalldämpfungsvorrichtung für eine Schiffs-Gasturbinenanlage
US4293053A (en) * 1979-12-18 1981-10-06 United Technologies Corporation Sound absorbing structure
GB2090334B (en) * 1980-12-29 1983-11-16 Rolls Royce Damping flutter of ducted fans
US4944362A (en) * 1988-11-25 1990-07-31 General Electric Company Closed cavity noise suppressor
US5291672A (en) * 1992-12-09 1994-03-08 General Electric Company Sound suppression mixer
JP3076945B2 (ja) * 1993-06-15 2000-08-14 松下電器産業株式会社 吸音装置
CH691191A5 (de) * 2000-01-06 2001-05-15 Rudolf Ing Htl Gehring Drehverbindung auf Gleitlagerbasis.
DE50110932D1 (de) 2000-12-08 2006-10-19 Alstom Technology Ltd Abgassystem mit Helmholtz-Resonator
GB2389150B (en) 2001-09-07 2004-08-25 Avon Polymer Prod Ltd Noise and vibration suppressors
US6669436B2 (en) 2002-02-28 2003-12-30 Dresser-Rand Company Gas compression apparatus and method with noise attenuation
US20050161280A1 (en) * 2002-12-26 2005-07-28 Fujitsu Limited Silencer and electronic equipment
US6918740B2 (en) * 2003-01-28 2005-07-19 Dresser-Rand Company Gas compression apparatus and method with noise attenuation
DE102004012929B3 (de) * 2004-03-17 2005-04-21 Dornier Gmbh Anordnung zur Lärmreduzierung in Turbofantriebwerken
US7337875B2 (en) * 2004-06-28 2008-03-04 United Technologies Corporation High admittance acoustic liner
US7497301B2 (en) * 2005-01-27 2009-03-03 Fleetguard, Inc. Tubular acoustic silencer
US7401682B2 (en) * 2005-08-10 2008-07-22 United Technologies Corporation Architecture for an acoustic liner
US7311175B2 (en) * 2005-08-10 2007-12-25 United Technologies Corporation Acoustic liner with bypass cooling
US8191678B2 (en) * 2006-01-19 2012-06-05 Se Electronics International, Inc. Apparatus for absorbing acoustical energy and use thereof
US7413053B2 (en) * 2006-01-25 2008-08-19 Siemens Power Generation, Inc. Acoustic resonator with impingement cooling tubes
US7870929B2 (en) * 2008-04-29 2011-01-18 The Boeing Company Engine assembly, acoustical liner and associated method of fabrication
WO2009137466A2 (fr) * 2008-05-05 2009-11-12 3M Innovative Properties Company Composite acoustique
US8028802B2 (en) * 2008-06-30 2011-10-04 General Electric Company Method and system for damped acoustic panels
US9404441B2 (en) * 2008-08-18 2016-08-02 Aerojet Rocketdyne Of De, Inc. Low velocity injector manifold for hypergolic rocket engine
US7857093B2 (en) * 2009-03-17 2010-12-28 Spirit Aerosystems, Inc. Engine inlet deep acoustic liner section
US20120247867A1 (en) * 2010-01-08 2012-10-04 Jun Yang Composite sound-absorbing device with built in resonant cavity
FR2960334B1 (fr) * 2010-05-19 2012-08-03 Snecma Panneau de traitement acoustique multicouches
KR101537120B1 (ko) * 2010-08-17 2015-07-16 현대중공업 주식회사 복합형 배기가스 소음기
US8973365B2 (en) 2010-10-29 2015-03-10 Solar Turbines Incorporated Gas turbine combustor with mounting for Helmholtz resonators
DE102011008920A1 (de) 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Schallabsorber, insbesondere für einen Gasturbinenabgaskonus und Verfahren zu dessen Herstellung
US8826669B2 (en) 2011-11-09 2014-09-09 Pratt & Whitney Canada Corp. Gas turbine exhaust case
US8944753B2 (en) 2011-11-09 2015-02-03 Pratt & Whitney Canada Corp. Strut mounting arrangement for gas turbine exhaust case
US9200537B2 (en) 2011-11-09 2015-12-01 Pratt & Whitney Canada Corp. Gas turbine exhaust case with acoustic panels
DE102011120979A1 (de) * 2011-12-13 2013-06-13 Rolls-Royce Deutschland Ltd & Co Kg Akustischer Absorber
US8763753B2 (en) 2012-02-10 2014-07-01 General Electric Company Acoustic panel and method of forming
CN104145105B (zh) * 2012-02-24 2017-03-01 三菱重工业株式会社 消音器、燃烧器及燃气涡轮
US8733500B1 (en) * 2012-11-12 2014-05-27 Hexcel Corporation Acoustic structure with internal thermal regulators
US8997923B2 (en) * 2013-08-12 2015-04-07 Hexcel Corporation Sound wave guide for use in acoustic structures
EP2881667B1 (fr) * 2013-10-11 2017-04-26 General Electric Technology GmbH Amortisseur de Helmholtz avec un joint refroidi à l'air pour une turbine à gaz
US20160017810A1 (en) * 2014-07-21 2016-01-21 United Technologies Corporation Acoustic liner heat exchanger
EP3186558B1 (fr) * 2014-08-26 2020-06-24 Siemens Energy, Inc. Agencement de trous de refroidissement de film pour résonateurs acoustiques dans des moteurs à turbine à gaz
DE102014218350A1 (de) 2014-09-12 2016-03-17 Rolls-Royce Deutschland Ltd & Co Kg Schalldämpfende Anordnung für eine Triebwerksgondel und Triebwerksgondel mit einer solchen Anordnung
US9783316B2 (en) * 2015-06-22 2017-10-10 Rohr, Inc. Acoustic panel assembly with a folding chamber
US9472179B1 (en) * 2015-09-05 2016-10-18 Xiaobing Cai Sound absorber
EP3182008A1 (fr) * 2015-12-18 2017-06-21 Ansaldo Energia IP UK Limited Amortisseur de helmholtz destiné à une turbine à gaz et une telle turbine avec ledit amortisseur
US9620102B1 (en) * 2016-05-02 2017-04-11 Hexcel Corporation Stepped acoustic structures with multiple degrees of freedom
US10472068B2 (en) 2016-07-12 2019-11-12 B/E Aerospace, Inc. Intermediate stowage retainer for aircraft monument storage bay
US10473120B2 (en) * 2017-03-09 2019-11-12 Denso International America, Inc. Blower assembly having resonators and resonator assembly
FR3065570B1 (fr) * 2017-04-21 2019-05-03 Office National D'etudes Et De Recherches Aerospatiales Garniture surfacique pour absorption acoustique
US10436118B2 (en) 2017-06-19 2019-10-08 Rohr, Inc. Acoustic panel with folding chamber
US10851713B2 (en) * 2017-08-29 2020-12-01 Mra Systems, Llc. Acoustic liner having internal structure
US10720136B2 (en) * 2017-12-04 2020-07-21 Zin Technologies, Inc. Layered chamber acoustic attenuation
US11541988B2 (en) 2017-12-20 2023-01-03 Airbus Canada Managing Gp Inc. Vibration-damped aircraft wheel bin
SE544189C2 (en) * 2018-02-13 2022-02-22 Faurecia Creo Ab Acoustic damper for a gas duct system
DE102018216215A1 (de) * 2018-09-24 2020-03-26 Mahle International Gmbh Luftleitungsrohr und eine Klimaanlage für ein Fahrzeug
JP7172457B2 (ja) * 2018-11-05 2022-11-16 ヤマハ株式会社 吸音用ユニットおよび吸音構造体
JP7310120B2 (ja) 2018-11-05 2023-07-19 ヤマハ株式会社 吸音構造体
EP3792188A1 (fr) * 2019-09-10 2021-03-17 RUAG Schweiz AG Agencement de protection acoustique modulaire et procédé de fabrication d'un tel agencement de protection acoustique
CN111105774A (zh) * 2019-10-29 2020-05-05 同济大学 亥姆霍兹共振器及基于其的低频宽带吸声降噪结构
US11415055B2 (en) * 2020-03-09 2022-08-16 Honeywell International Inc. Alternating helicoid cell structure and methods of producing the same
FR3111003A1 (fr) * 2020-05-29 2021-12-03 Airbus Operations Structure alvéolaire d’insonorisation incluant un diaphragme muni d’un tube configuré pour traiter différentes fréquences acoustiques, procédé de fabrication d'une telle structure, et outil associé

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2249769A1 (fr) * 1973-10-31 1975-05-30 Rolls Royce
FR2260059A1 (fr) * 1974-02-01 1975-08-29 Brunswick Corp
US3910374A (en) * 1974-03-18 1975-10-07 Rohr Industries Inc Low frequency structural acoustic attenuator
US3948346A (en) * 1974-04-02 1976-04-06 Mcdonnell Douglas Corporation Multi-layered acoustic liner

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3819009A (en) * 1973-02-01 1974-06-25 Gen Electric Duct wall acoustic treatment
US3850261A (en) * 1973-03-01 1974-11-26 Gen Electric Wide band width single layer sound suppressing panel

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2249769A1 (fr) * 1973-10-31 1975-05-30 Rolls Royce
FR2260059A1 (fr) * 1974-02-01 1975-08-29 Brunswick Corp
US3910374A (en) * 1974-03-18 1975-10-07 Rohr Industries Inc Low frequency structural acoustic attenuator
US3948346A (en) * 1974-04-02 1976-04-06 Mcdonnell Douglas Corporation Multi-layered acoustic liner

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0219218A1 (fr) * 1985-09-05 1987-04-22 AlliedSignal Inc. Dispositif d'insonorisation
FR2588614A1 (fr) * 1985-10-16 1987-04-17 Nuovo Pignone Spa Silencieux d'echappement pour turbine a gaz de forte puissance.
FR2685386A1 (fr) * 1991-12-20 1993-06-25 Europ Propulsion Systeme d'amortissement des instabilites de combustion haute frequence dans une chambre de combustion.
EP0549402A1 (fr) * 1991-12-20 1993-06-30 Societe Europeenne De Propulsion Système d'amortissement des instabilités de combustion haute fréquence dans une chambre de combustion
US5353598A (en) * 1991-12-20 1994-10-11 Societe Europeenne De Propulsion Damping system for high frequency combustion instabilities in a combustion chamber
EP1849974A2 (fr) * 2006-04-27 2007-10-31 United Technologies Corporation Résonateur de pointe arrière pour moteur de turbine
EP1849974A3 (fr) * 2006-04-27 2010-11-03 United Technologies Corporation Résonateur de pointe arrière pour moteur de turbine
EP2484881A1 (fr) * 2006-04-27 2012-08-08 United Technologies Corporation Cône arrière résonateur d'une turbine à gaz
DE102015117092A1 (de) 2013-11-13 2016-04-21 Ge Energy Products France Snc Thermoakustische Schutzstruktur für eine rotierende Maschine
FR3065754A1 (fr) * 2017-04-28 2018-11-02 Safran Aircraft Engines Cellule d'absorption acoustique pour turboreacteur et panneau de traitement acoustique associe
US10557417B2 (en) 2017-04-28 2020-02-11 Safran Aircraft Engines Acoustic absorber cell for a turbojet, and an associated acoustic treatment panel

Also Published As

Publication number Publication date
JPS5314213A (en) 1978-02-08
GB1520720A (en) 1978-08-09
FR2356820B1 (fr) 1983-05-20
US4106587A (en) 1978-08-15
IT1083790B (it) 1985-05-25
DE2729568A1 (de) 1978-01-12
JPS6014893B2 (ja) 1985-04-16

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Legal Events

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