DE3866412D1 - Akustische platte fuer schalldaempfendes futter und strahlvortriebsturbine mit einem solchen futter. - Google Patents

Akustische platte fuer schalldaempfendes futter und strahlvortriebsturbine mit einem solchen futter.

Info

Publication number
DE3866412D1
DE3866412D1 DE8888400766T DE3866412T DE3866412D1 DE 3866412 D1 DE3866412 D1 DE 3866412D1 DE 8888400766 T DE8888400766 T DE 8888400766T DE 3866412 T DE3866412 T DE 3866412T DE 3866412 D1 DE3866412 D1 DE 3866412D1
Authority
DE
Germany
Prior art keywords
lining
sound
drive turbine
acoustic panel
jet drive
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.)
Expired - Lifetime
Application number
DE8888400766T
Other languages
English (en)
Inventor
Pascal Jean-Louis Marie Autie
Philippe Pierre Avignon
Dominique Paul Camusso
Alexandre Forestier
Gilles Ulryck Gilles Ulryck
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3866412D1 publication Critical patent/DE3866412D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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)
  • Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
DE8888400766T 1987-04-08 1988-03-30 Akustische platte fuer schalldaempfendes futter und strahlvortriebsturbine mit einem solchen futter. Expired - Lifetime DE3866412D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8704908A FR2613773B1 (fr) 1987-04-08 1987-04-08 Panneau acoustique pour garniture insonorisante et turboreacteur comportant une telle garniture

Publications (1)

Publication Number Publication Date
DE3866412D1 true DE3866412D1 (de) 1992-01-09

Family

ID=9349890

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888400766T Expired - Lifetime DE3866412D1 (de) 1987-04-08 1988-03-30 Akustische platte fuer schalldaempfendes futter und strahlvortriebsturbine mit einem solchen futter.

Country Status (5)

Country Link
US (1) US4858721A (de)
EP (1) EP0289376B1 (de)
JP (1) JPS63272924A (de)
DE (1) DE3866412D1 (de)
FR (1) FR2613773B1 (de)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4217767C1 (de) * 1992-05-29 1993-08-26 Deutsche Aerospace Ag, 8000 Muenchen, De
US6309176B1 (en) * 1999-11-12 2001-10-30 Siemens Automotive Inc. Noise attenuating sound resonator for automotive cooling module shroud
US6669436B2 (en) 2002-02-28 2003-12-30 Dresser-Rand Company Gas compression apparatus and method with noise attenuation
GB0206136D0 (en) * 2002-03-15 2002-04-24 Rolls Royce Plc Improvements in or relating to cellular materials
US6918740B2 (en) * 2003-01-28 2005-07-19 Dresser-Rand Company Gas compression apparatus and method with noise attenuation
US7337875B2 (en) * 2004-06-28 2008-03-04 United Technologies Corporation High admittance acoustic liner
US7552796B2 (en) * 2006-04-27 2009-06-30 United Technologies Corporation Turbine engine tailcone resonator
US8028791B2 (en) * 2007-05-22 2011-10-04 Owens Corning Intellectual Capital, Llc Sound reflective acoustic panel
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.
FR2919347B1 (fr) * 2007-07-26 2009-11-20 Snecma Enveloppe externe de conduite de soufflante dans une turbomachine.
FR2920136B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Systeme de liaison entre une structure interne et un structure externe d'une nacelle
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
US20100240295A1 (en) * 2009-03-20 2010-09-23 Salman Akhtar Air handling system
DE102009037956B4 (de) 2009-08-18 2024-06-06 MTU Aero Engines AG Turbinenaustrittsgehäuse
FR2965859B1 (fr) * 2010-10-07 2012-11-02 Snecma Dispositif de traitement acoustique du bruit emis par un turboreacteur
FR2975735A1 (fr) 2011-05-27 2012-11-30 Snecma Carter de soufflante de turbomachine et procede pour sa fabrication
FR2980241A1 (fr) * 2011-09-15 2013-03-22 Snecma Panneau acoustique
US9850850B2 (en) * 2013-10-23 2017-12-26 Rohr, Inc. Acoustically treated thrust reverser track beam
GB201400179D0 (en) 2014-01-06 2014-02-19 Mbda Uk Ltd Structure for controlling the aero-acoustic environment in an aircraft weapons bay
FR3016187B1 (fr) 2014-01-09 2016-01-01 Snecma Protection contre le feu d'un carter de soufflante en materiau composite
FR3028886B1 (fr) * 2014-11-24 2019-09-13 Safran Aircraft Engines Organe de reduction de bruit de soufflante de turboreacteur
US10107307B2 (en) 2015-04-14 2018-10-23 Pratt & Whitney Canada Corp. Gas turbine engine rotor casing treatment
US10371173B2 (en) * 2015-05-07 2019-08-06 United Technologies Corporation Liner for a gas turbine engine
US10161357B2 (en) 2016-06-17 2018-12-25 Rohr, Inc. Acoustically treated thrust reverser track beam
US20180029719A1 (en) * 2016-07-28 2018-02-01 The Boeing Company Drag reducing liner assembly and methods of assembling the same
GB201720603D0 (en) 2017-12-11 2018-01-24 Rolls Royce Plc Fairings for power generation machines
GB201802768D0 (en) * 2018-02-21 2018-04-04 Rolls Royce Plc Fairings for power generation machines
US11414203B2 (en) * 2018-09-28 2022-08-16 Rohr, Inc. Active laminar flow control plenum panel arrangement
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
CN111312202B (zh) * 2018-12-11 2024-03-08 上海汽车集团股份有限公司 一种消声设备
FR3097261B1 (fr) 2019-06-13 2021-05-28 Safran Aircraft Engines Ensemble support d’une sonde dans une turbomachine pour aéronef
RU203213U1 (ru) * 2020-07-08 2021-03-26 Государственное предприятие "Запорожское машиностроительное конструкторское бюро "Прогресс" имени академика А.Г. Ивченко Звукопоглощающая конструкция для тракта турбореактивного двухконтурного двигателя
US11460048B2 (en) 2020-12-18 2022-10-04 Rohr, Inc. Attachable acoustic panels and method of making same
US11753968B2 (en) * 2021-08-23 2023-09-12 Rolls-Royce Deutschland Ltd & Co Kg Nacelle cowling structure for a turbomachine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR57621E (de) * 1953-03-20
US4258823A (en) * 1979-01-02 1981-03-31 The Boeing Company Inflow turbulence control structure
FR2498793A1 (fr) * 1981-01-29 1982-07-30 Snecma Garniture insonorisante pour conduit de gaz notamment pour veine de soufflante de turboreacteur et outillage pour sa fabrication
US4433751A (en) * 1981-12-09 1984-02-28 Pratt & Whitney Aircraft Of Canada Limited Sound suppressor liner
US4452335A (en) * 1982-05-03 1984-06-05 United Technologies Corporation Sound absorbing structure for a gas turbine engine
US4751979A (en) * 1985-05-16 1988-06-21 Airborne Express, Inc. Engine noise suppression kit for the nacelles of a jet aircraft

Also Published As

Publication number Publication date
EP0289376B1 (de) 1991-11-27
FR2613773B1 (fr) 1990-11-30
EP0289376A1 (de) 1988-11-02
JPH0478826B2 (de) 1992-12-14
FR2613773A1 (fr) 1988-10-14
US4858721A (en) 1989-08-22
JPS63272924A (ja) 1988-11-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee