FR2261583A1 - - Google Patents

Info

Publication number
FR2261583A1
FR2261583A1 FR7504695A FR7504695A FR2261583A1 FR 2261583 A1 FR2261583 A1 FR 2261583A1 FR 7504695 A FR7504695 A FR 7504695A FR 7504695 A FR7504695 A FR 7504695A FR 2261583 A1 FR2261583 A1 FR 2261583A1
Authority
FR
France
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
FR7504695A
Other versions
FR2261583B1 (fr
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 FR2261583A1 publication Critical patent/FR2261583A1/fr
Application granted granted Critical
Publication of FR2261583B1 publication Critical patent/FR2261583B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/663—Sound attenuation
    • F04D29/664—Sound attenuation by means of sound absorbing material
    • 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
    • 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
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
FR7504695A 1974-02-15 1975-02-14 Expired FR2261583B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US442893A US3890060A (en) 1974-02-15 1974-02-15 Acoustic duct with asymmetric acoustical treatment

Publications (2)

Publication Number Publication Date
FR2261583A1 true FR2261583A1 (fr) 1975-09-12
FR2261583B1 FR2261583B1 (fr) 1981-02-13

Family

ID=23758566

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7504695A Expired FR2261583B1 (fr) 1974-02-15 1975-02-14

Country Status (7)

Country Link
US (1) US3890060A (fr)
JP (1) JPS6010168B2 (fr)
BE (1) BE825517A (fr)
DE (1) DE2504073C2 (fr)
FR (1) FR2261583B1 (fr)
GB (1) GB1499724A (fr)
IT (1) IT1031366B (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2820715A1 (fr) 2001-02-15 2002-08-16 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR2820716A1 (fr) 2001-02-15 2002-08-16 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
WO2019158884A1 (fr) * 2018-02-19 2019-08-22 Safran Aircraft Engines Nacelle de turbomachine à parois acoustiquement poreuses

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1483590A (en) * 1973-12-27 1977-08-24 Chrysler Uk Fan assemblies
US4104002A (en) * 1976-12-02 1978-08-01 General Electric Company Spiral strip acoustic treatment
US4989886A (en) * 1988-12-30 1991-02-05 Textron Inc. Braided filamentary sealing element
US5029875A (en) * 1989-07-07 1991-07-09 Textron Inc. Fluid seal structure
JP2630652B2 (ja) * 1989-08-09 1997-07-16 三菱電機ホーム機器株式会社 送風機
US5594218A (en) * 1995-01-04 1997-01-14 Northrop Grumman Corporation Anechoic chamber absorber and method
US5709529A (en) * 1995-11-14 1998-01-20 Westinghouse Electric Corporation Optimization of turbomachinery harmonics
US5702231A (en) * 1996-08-09 1997-12-30 The Boeing Company Apparatus and method for reducing noise emissions from a gas turbine engine inlet
FR2787513B1 (fr) 1998-12-17 2001-01-19 Turbomeca Dispositif d'echappement multicanal de turbomachine traite acoustiquement
SE515528C2 (sv) * 1999-12-07 2001-08-20 Saab Ab Anordning vid en akustisk absorbent
US6557799B1 (en) 2001-11-09 2003-05-06 The Boeing Company Acoustic treated thrust reverser bullnose fairing assembly
GB2385378B (en) * 2002-02-14 2005-08-31 Rolls Royce Plc Engine casing
FR2898870B1 (fr) * 2006-03-24 2008-05-23 Aircelle Sa Structure de virole d'entree d'air
GB0608236D0 (en) * 2006-04-26 2006-06-07 Rolls Royce Plc Aeroengine noise reduction
FR2905734B1 (fr) * 2006-09-07 2012-07-13 Airbus France Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef
US8780550B2 (en) * 2006-09-26 2014-07-15 Hewlett-Packard Development Company, L.P. Dampening acoustic vibrations within an electronic system
US20080110695A1 (en) * 2006-11-15 2008-05-15 Mc Clellan W Thomas High efficiency, frequency-tunable, acoustic wool and method of attenuating acoustic vibrations
DE102007019762A1 (de) * 2007-04-25 2008-10-30 Eads Deutschland Gmbh Schallschutzvorrichtung für ein Strahltriebwerk oder eine Turbine
JP2009062977A (ja) * 2007-08-15 2009-03-26 Rohr Inc 線形音響ライナー
FR2926704B1 (fr) * 2008-01-25 2013-02-01 Velecta Paramount Silencieux pour appareil de sechage et seche-cheveux silencieux
DE102011006273A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Rotor einer Axialverdichterstufe einer Turbomaschine
DE102011006275A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Stator einer Axialverdichterstufe einer Turbomaschine
DE102011007767A1 (de) * 2011-04-20 2012-10-25 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine
US8943792B2 (en) * 2011-06-29 2015-02-03 United Technologies Corporation Gas-driven propulsor with tip turbine fan
DE102011056826B4 (de) 2011-12-21 2014-06-26 Eads Deutschland Gmbh Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung
US9476385B2 (en) * 2012-11-12 2016-10-25 The Boeing Company Rotational annular airscrew with integrated acoustic arrester
EP4036388A1 (fr) 2013-02-26 2022-08-03 Raytheon Technologies Corporation Traitement acoustique pour atténuer le bruit de ventilateur
EP4019754A1 (fr) 2013-03-15 2022-06-29 Raytheon Technologies Corporation Revêtement acoustique ayant des caractéristiques variées
WO2015023325A1 (fr) * 2013-08-12 2015-02-19 United Technologies Corporation Trajectoire de flux de ventilateur non axisymétrique
US9850850B2 (en) * 2013-10-23 2017-12-26 Rohr, Inc. Acoustically treated thrust reverser track beam
DE102014006112A1 (de) * 2014-04-29 2015-10-29 Autogyro Ag Luftfahrzeug
AU2016267963B2 (en) 2015-05-25 2020-08-13 Dotterel Technologies Limited A shroud for an aircraft
US9771868B2 (en) * 2015-07-21 2017-09-26 The Boeing Company Sound attenuation apparatus and method
US9587563B2 (en) 2015-07-21 2017-03-07 The Boeing Company Sound attenuation apparatus and method
US10823060B2 (en) * 2015-12-18 2020-11-03 Raytheon Technologies Corporation Gas turbine engine with short inlet, acoustic treatment and anti-icing features
US10161357B2 (en) 2016-06-17 2018-12-25 Rohr, Inc. Acoustically treated thrust reverser track beam
CN110997486A (zh) 2017-07-24 2020-04-10 多特瑞尔技术有限公司 护罩
WO2019221613A1 (fr) 2018-05-16 2019-11-21 Dotterel Technologies Limited Systèmes et procédés de capture audio
DE102018116062A1 (de) * 2018-07-03 2020-01-09 Rolls-Royce Deutschland Ltd & Co Kg Strukturbaugruppe für einen Verdichter einer Strömungsmaschine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2909235A (en) * 1955-11-03 1959-10-20 Gen Dynamics Corp Muffler
US3263771A (en) * 1964-05-21 1966-08-02 Seifert Kurt Sound absorbing pipe lining having packing with different densities
US3542152A (en) * 1968-04-08 1970-11-24 Gen Electric Sound suppression panel
FR1580553A (fr) * 1968-07-26 1969-09-05
US3508838A (en) * 1968-09-16 1970-04-28 Gen Electric Sound suppression of compressors used in gas turbine engines
US3655008A (en) * 1971-01-28 1972-04-11 Rohr Corp Sound suppressing apparatus

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2820715A1 (fr) 2001-02-15 2002-08-16 Eads Airbus Sa Procede de degivrage d'un capot d'entree d'air de moteur a reaction et dispositif pour sa mise en oeuvre
FR2820716A1 (fr) 2001-02-15 2002-08-16 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
EP1232944A1 (fr) 2001-02-15 2002-08-21 AIRBUS FRANCE (Société par Actions Simplifiée) Procédé de dégivrage par circulation forcée d'un fluide, d'un capot d'entrée d'air de moteur à réaction et dispositif pour sa mise en oeuvre
EP1232945A1 (fr) 2001-02-15 2002-08-21 AIRBUS FRANCE (Société par Actions Simplifiée) Procédé de dégivrage d'un capot d'entrée d'air de moteur à réaction et dispositif pour sa mise en oeuvre
WO2019158884A1 (fr) * 2018-02-19 2019-08-22 Safran Aircraft Engines Nacelle de turbomachine à parois acoustiquement poreuses
FR3078107A1 (fr) * 2018-02-19 2019-08-23 Safran Aircraft Engines Nacelle de turbomachine a parois acoustiquement poreuses
US11472565B2 (en) 2018-02-19 2022-10-18 Safran Aircraft Engines Turbomachine nacelle having acoustically porous walls

Also Published As

Publication number Publication date
US3890060A (en) 1975-06-17
DE2504073C2 (de) 1983-12-01
BE825517A (fr) 1975-05-29
GB1499724A (en) 1978-02-01
DE2504073A1 (de) 1975-08-21
FR2261583B1 (fr) 1981-02-13
JPS50118114A (fr) 1975-09-16
JPS6010168B2 (ja) 1985-03-15
IT1031366B (it) 1979-04-30

Similar Documents

Publication Publication Date Title
FR2261583B1 (fr)
FR2275243B1 (fr)
FR2273004B2 (fr)
JPS5153109A (fr)
FR2262115A1 (fr)
FR2260408A1 (fr)
JPS50139134A (fr)
JPS50134314U (fr)
JPS50142585U (fr)
FR2257674A1 (fr)
FR2261927B1 (fr)
CS171565B1 (fr)
JPS50117651U (fr)
JPS50111328U (fr)
JPS50111082U (fr)
JPS50102340U (fr)
CH583799A5 (fr)
CH580484A5 (fr)
CH600504A5 (fr)
CH585442A5 (fr)
CH583955A5 (fr)
CH583833A5 (fr)
CH580825A5 (fr)
CH583448A5 (fr)
CH583329B5 (fr)