JPS53123714A - Axial flow machinery - Google Patents

Axial flow machinery

Info

Publication number
JPS53123714A
JPS53123714A JP3895677A JP3895677A JPS53123714A JP S53123714 A JPS53123714 A JP S53123714A JP 3895677 A JP3895677 A JP 3895677A JP 3895677 A JP3895677 A JP 3895677A JP S53123714 A JPS53123714 A JP S53123714A
Authority
JP
Japan
Prior art keywords
axial flow
flow machinery
machinery
axial
flow
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
JP3895677A
Other languages
English (en)
Other versions
JPS574814B2 (ja
Inventor
Uirufuoodo Rourii Buraian
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of JPS53123714A publication Critical patent/JPS53123714A/ja
Publication of JPS574814B2 publication Critical patent/JPS574814B2/ja
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
    • 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
    • F02C7/24—Heat or noise insulation
    • 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
    • F04D29/665—Sound attenuation by means of resonance chambers or interference

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP3895677A 1976-04-05 1977-04-05 Axial flow machinery Granted JPS53123714A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13739/76A GB1522558A (en) 1976-04-05 1976-04-05 Duct linings

Publications (2)

Publication Number Publication Date
JPS53123714A true JPS53123714A (en) 1978-10-28
JPS574814B2 JPS574814B2 (ja) 1982-01-27

Family

ID=10028496

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3895677A Granted JPS53123714A (en) 1976-04-05 1977-04-05 Axial flow machinery

Country Status (6)

Country Link
US (1) US4122672A (ja)
JP (1) JPS53123714A (ja)
DE (1) DE2715295A1 (ja)
FR (1) FR2347539A1 (ja)
GB (1) GB1522558A (ja)
IT (1) IT1075717B (ja)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1185101A (en) * 1980-03-03 1985-04-09 Daniel J. Lahti Drag-reducing nacelle
GB2076049B (en) * 1980-05-17 1983-10-26 Rolls Royce Variable acoustic impedance lining
GB2090334B (en) * 1980-12-29 1983-11-16 Rolls Royce Damping flutter of ducted fans
FR2603350B1 (fr) * 1986-09-02 1991-03-29 Cogema Ventilateur helicoide a gaine de guidage
IT1217607B (it) * 1988-05-16 1990-03-30 Riello Condizionatori Spa Motoventilatore centrifugo particolarmente silvenzioso
GB8822798D0 (en) * 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine
GB9014381D0 (en) * 1990-06-28 1990-08-22 Short Brothers Plc A composite structural component
DE4340951A1 (de) * 1992-12-04 1994-06-09 Grumman Aerospace Corp Einstückiges Triebwerkeinlaß-Schallrohr
FR2787513B1 (fr) * 1998-12-17 2001-01-19 Turbomeca Dispositif d'echappement multicanal de turbomachine traite acoustiquement
GB2361035A (en) * 2000-04-07 2001-10-10 Rolls Royce Plc Gas turbine engine vane with noise attenuation features
GB0119608D0 (en) 2001-08-11 2001-10-03 Rolls Royce Plc A guide vane assembly
US6557799B1 (en) 2001-11-09 2003-05-06 The Boeing Company Acoustic treated thrust reverser bullnose fairing assembly
FR2847304B1 (fr) * 2002-11-18 2005-07-01 Airbus France Nacelle de reacteur d'aeronef a attenuation acoustique
US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
DE602004014154D1 (de) * 2003-07-29 2008-07-10 Pratt & Whitney Canada Turbofan-Triebwerksgehäuse, Turbofantriebwerk und entsprechendes Verfahren
DE102004012929B3 (de) * 2004-03-17 2005-04-21 Dornier Gmbh Anordnung zur Lärmreduzierung in Turbofantriebwerken
GB0415844D0 (en) 2004-07-15 2004-08-18 Rolls Royce Plc Noise control
US7707708B2 (en) * 2005-09-21 2010-05-04 Rohr, Inc. Apparatus for making a tubular composite structure
US7861823B2 (en) * 2005-11-04 2011-01-04 United Technologies Corporation Duct for reducing shock related noise
FR2898940B1 (fr) * 2006-03-24 2008-05-30 Snecma Sa Corps central de tuyere de turboreacteur
GB0608236D0 (en) * 2006-04-26 2006-06-07 Rolls Royce Plc Aeroengine noise reduction
FR2901578B1 (fr) * 2006-05-23 2008-07-25 Snecma Sa Corps central pour canal d'echappement d'un turboreacteur, turboreacteur
US8347633B2 (en) 2007-07-27 2013-01-08 United Technologies Corporation Gas turbine engine with variable geometry fan exit guide vane system
US8459035B2 (en) 2007-07-27 2013-06-11 United Technologies Corporation Gas turbine engine with low fan pressure ratio
US7640961B2 (en) * 2008-03-21 2010-01-05 Rohr, Inc. Apparatus and method for making a tubular composite barrel
FR2930764B1 (fr) * 2008-04-30 2010-05-07 Airbus France Panneau d'attenuation d'ondes intercale entre une motorisation et une entree d'air d'une nacelle d'aeronef
US8025499B2 (en) 2008-11-03 2011-09-27 Rohr, Inc. Multi-segment tool and method for composite formation
FR2941495B1 (fr) * 2009-01-27 2017-09-29 Turbomeca Conduit d'echappement insonorise pour turbomoteur
US7857093B2 (en) * 2009-03-17 2010-12-28 Spirit Aerosystems, Inc. Engine inlet deep acoustic liner section
GB0908128D0 (en) 2009-05-12 2009-06-24 Rolls Royce Plc An intake duct liner for a turbofan gas turbine engine
US8820088B2 (en) 2010-07-27 2014-09-02 United Technologies Corporation Variable area fan nozzle with acoustic system for a gas turbine engine
GB2483060B (en) * 2010-08-23 2013-05-15 Rolls Royce Plc A turbomachine casing assembly
US9957840B2 (en) * 2013-02-26 2018-05-01 United Technologies Corporation Acoustic treatment to mitigate fan noise
EP2971659B1 (en) 2013-03-15 2021-09-22 Raytheon Technologies Corporation Acoustic liner with varied properties
FR3007064B1 (fr) 2013-06-13 2018-06-29 Composite Industrie Secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece
FR3007063B1 (fr) * 2013-06-13 2015-07-03 Composite Ind Piece de materiau abradable pour la fabrication d'un secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece
EP2913270B1 (en) 2014-02-28 2016-02-24 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotorcraft with at least one main rotor and at least one counter-torque rotor
EP2913271A1 (en) 2014-02-28 2015-09-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotorcraft with at least one main rotor and at least one counter-torque rotor
EP2913269B1 (en) 2014-02-28 2019-01-16 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotorcraft with at least one main rotor and at least one counter-torque rotor
US9783316B2 (en) 2015-06-22 2017-10-10 Rohr, Inc. Acoustic panel assembly with a folding chamber
GB201511454D0 (en) 2015-06-30 2015-08-12 Rolls Royce Plc Aircraft engine nacelle
US20180135515A1 (en) * 2016-11-17 2018-05-17 General Electric Company System and method for fluid acoustic treatment
US10436118B2 (en) 2017-06-19 2019-10-08 Rohr, Inc. Acoustic panel with folding chamber
DE102020201417A1 (de) 2020-02-05 2021-08-05 kopter germany GmbH Rotorsystem für ein Fluggerät
DE102021200287A1 (de) 2021-01-14 2022-07-14 MTU Aero Engines AG Zellenartiger Belag und Schaufelanordnung für eine Turbomaschine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3439774A (en) * 1966-01-21 1969-04-22 Boeing Co Sound energy absorbing apparatus
US3542152A (en) * 1968-04-08 1970-11-24 Gen Electric Sound suppression panel
US3508838A (en) * 1968-09-16 1970-04-28 Gen Electric Sound suppression of compressors used in gas turbine engines
US3821999A (en) * 1972-09-05 1974-07-02 Mc Donnell Douglas Corp Acoustic liner
US3913702A (en) * 1973-06-04 1975-10-21 Lockheed Aircraft Corp Cellular sound absorptive structure
US3948346A (en) * 1974-04-02 1976-04-06 Mcdonnell Douglas Corporation Multi-layered acoustic liner
CA1027002A (en) * 1974-08-30 1978-02-28 Horst W.W. Hehmann Phased treatment noise suppressor for acoustic duct applications
US3937590A (en) * 1974-09-03 1976-02-10 General Electric Company Acoustic duct with peripherally segmented acoustic treatment

Also Published As

Publication number Publication date
DE2715295B2 (ja) 1979-11-22
FR2347539B1 (ja) 1984-05-11
IT1075717B (it) 1985-04-22
DE2715295A1 (de) 1977-10-13
DE2715295C3 (ja) 1980-07-31
JPS574814B2 (ja) 1982-01-27
GB1522558A (en) 1978-08-23
US4122672A (en) 1978-10-31
FR2347539A1 (fr) 1977-11-04

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