DE69524551D1 - Bläser fur ein Turbostrahltriebwerk - Google Patents

Bläser fur ein Turbostrahltriebwerk

Info

Publication number
DE69524551D1
DE69524551D1 DE69524551T DE69524551T DE69524551D1 DE 69524551 D1 DE69524551 D1 DE 69524551D1 DE 69524551 T DE69524551 T DE 69524551T DE 69524551 T DE69524551 T DE 69524551T DE 69524551 D1 DE69524551 D1 DE 69524551D1
Authority
DE
Germany
Prior art keywords
blower
jet engine
turbo jet
turbo
engine
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 - Fee Related
Application number
DE69524551T
Other languages
English (en)
Other versions
DE69524551T2 (de
Inventor
Philip Roger Gliebe
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 DE69524551D1 publication Critical patent/DE69524551D1/de
Application granted granted Critical
Publication of DE69524551T2 publication Critical patent/DE69524551T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/045Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/175Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
    • G10K11/178Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
    • G10K11/1785Methods, e.g. algorithms; Devices
    • G10K11/17857Geometric disposition, e.g. placement of microphones
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/175Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
    • G10K11/178Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
    • G10K11/1785Methods, e.g. algorithms; Devices
    • G10K11/17861Methods, e.g. algorithms; Devices using additional means for damping sound, e.g. using sound absorbing panels
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/175Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
    • G10K11/178Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
    • G10K11/1787General system configurations
    • G10K11/17875General system configurations using an error signal without a reference signal, e.g. pure feedback
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/175Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound
    • G10K11/178Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using interference effects; Masking sound by electro-acoustically regenerating the original acoustic waves in anti-phase
    • G10K11/1787General system configurations
    • G10K11/17879General system configurations using both a reference signal and an error signal
    • G10K11/17881General system configurations using both a reference signal and an error signal the reference signal being an acoustic signal, e.g. recorded with a microphone
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286Arrangements 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/327Application in turbines in gas turbines to drive shrouded, high solidity propeller
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • F05D2260/962Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/10Applications
    • G10K2210/107Combustion, e.g. burner noise control of jet engines
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/10Applications
    • G10K2210/112Ducts
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/10Applications
    • G10K2210/121Rotating machines, e.g. engines, turbines, motors; Periodic or quasi-periodic signals in general
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/30Means
    • G10K2210/301Computational
    • G10K2210/3032Harmonics or sub-harmonics
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/30Means
    • G10K2210/301Computational
    • G10K2210/3045Multiple acoustic inputs, single acoustic output
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/30Means
    • G10K2210/321Physical
    • G10K2210/3217Collocated sensor and cancelling actuator, e.g. "virtual earth" designs
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/50Miscellaneous
    • G10K2210/509Hybrid, i.e. combining different technologies, e.g. passive and active
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/50Miscellaneous
    • G10K2210/511Narrow band, e.g. implementations for single frequency cancellation
DE69524551T 1994-11-28 1995-11-03 Bläser fur ein Turbostrahltriebwerk Expired - Fee Related DE69524551T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/345,094 US5478199A (en) 1994-11-28 1994-11-28 Active low noise fan assembly

Publications (2)

Publication Number Publication Date
DE69524551D1 true DE69524551D1 (de) 2002-01-24
DE69524551T2 DE69524551T2 (de) 2002-08-29

Family

ID=23353489

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69524551T Expired - Fee Related DE69524551T2 (de) 1994-11-28 1995-11-03 Bläser fur ein Turbostrahltriebwerk

Country Status (3)

Country Link
US (1) US5478199A (de)
EP (1) EP0715066B1 (de)
DE (1) DE69524551T2 (de)

Families Citing this family (78)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69523056T2 (de) * 1994-07-28 2002-02-07 Boeing Co Aktive kontrolle von bläsergeräusch in gasturbinenkanälen
US6201872B1 (en) * 1995-03-12 2001-03-13 Hersh Acoustical Engineering, Inc. Active control source cancellation and active control Helmholtz resonator absorption of axial fan rotor-stator interaction noise
JP2939940B2 (ja) 1996-07-09 1999-08-25 日本電気株式会社 ファン音消音装置
US5961067A (en) * 1996-09-10 1999-10-05 Allison Engine Company Method for reducing turboprop noise
US5845236A (en) * 1996-10-16 1998-12-01 Lord Corporation Hybrid active-passive noise and vibration control system for aircraft
US5919029A (en) * 1996-11-15 1999-07-06 Northrop Grumman Corporation Noise absorption system having active acoustic liner
JPH11247605A (ja) 1997-12-26 1999-09-14 United Technol Corp <Utc> タ―ボマシ―ンコンポ―ネントの振動緩衝方法及び装置
EP1099050B1 (de) * 1998-07-22 2002-10-23 Friedmund Nagel Vorrichtung und verfahren zur aktiven reduzierung der schallemission von strahltriebwerken und zu deren diagnose
US6405794B1 (en) * 1999-03-07 2002-06-18 Korea Institute Of Science And Technology Acoustic convection apparatus
US6901147B1 (en) * 1999-06-29 2005-05-31 Kabushiki Kaisha Toshiba Three-dimension active silencer
US6353789B1 (en) * 1999-12-13 2002-03-05 United Technologies Corporation Predicting broadband noise from a stator vane of a gas turbine engine
CA2293076C (en) * 1999-12-22 2010-03-30 Man-Chun Tse Fan and compressor noise attenuation
US6457941B1 (en) 2001-03-13 2002-10-01 The United States Of America As Represented By The Secretary Of The Navy Fan rotor with construction and safety performance optimization
US6386830B1 (en) 2001-03-13 2002-05-14 The United States Of America As Represented By The Secretary Of The Navy Quiet and efficient high-pressure fan assembly
US7059820B2 (en) * 2002-07-19 2006-06-13 Honeywell International, Inc. Noise control
US6655632B1 (en) 2002-08-27 2003-12-02 General Electric Company System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine
US20040244357A1 (en) * 2003-06-05 2004-12-09 Sloan Mark L. Divergent chevron nozzle and method
US6920958B2 (en) * 2003-10-17 2005-07-26 The Boeing Company Annular acoustic panel
JP4273926B2 (ja) * 2003-10-29 2009-06-03 株式会社日立製作所 消音装置及びそれを用いたプロジェクタ装置
US20050201567A1 (en) * 2004-03-12 2005-09-15 Browne Alan L. Tunable exhaust system
DE102004016246A1 (de) * 2004-04-02 2005-10-20 Mtu Aero Engines Gmbh Turbine, insbesondere Niederdruckturbine, einer Gasturbine, insbesondere eines Flugtriebwerks
US7095221B2 (en) * 2004-05-27 2006-08-22 Siemens Aktiengesellschaft Doppler radar sensing system for monitoring turbine generator components
US8757965B2 (en) * 2004-06-01 2014-06-24 Volvo Aero Corporation Gas turbine compression system and compressor structure
GB0415844D0 (en) * 2004-07-15 2004-08-18 Rolls Royce Plc Noise control
US7374403B2 (en) * 2005-04-07 2008-05-20 General Electric Company Low solidity turbofan
US7476086B2 (en) * 2005-04-07 2009-01-13 General Electric Company Tip cambered swept blade
FR2885955B1 (fr) * 2005-05-18 2007-06-22 Airbus France Sas Procede pour reduire les emissions sonores a l'arriere d'un turbomoteur et turbomoteur ainsi perfectionne.
GB0608236D0 (en) * 2006-04-26 2006-06-07 Rolls Royce Plc Aeroengine noise reduction
US7891464B2 (en) * 2006-06-15 2011-02-22 Hewlett-Packard Development, L.P. System and method for noise suppression
US7779960B2 (en) * 2006-08-18 2010-08-24 Hewlett-Packard Development Company, L.P. System and method for noise suppression
WO2008090544A2 (en) * 2007-01-22 2008-07-31 Silentium Ltd. Quiet fan incorporating active noise control (anc)
US20080273961A1 (en) 2007-03-05 2008-11-06 Rosenkrans William E Flutter sensing and control system for a gas turbine engine
TWI413492B (zh) * 2007-07-10 2013-10-21 Delta Electronics Inc 具有感測元件承載結構之風扇及其扇框
FR2932160B1 (fr) * 2008-06-06 2010-11-26 Airbus France Support d'appareils de mesure intercale entre une motorisation et une entree d'air d'une nacelle d'aeronef
US8331577B2 (en) * 2008-07-03 2012-12-11 Hewlett-Packard Development Company, L.P. Electronic device having active noise control with an external sensor
FR2965859B1 (fr) * 2010-10-07 2012-11-02 Snecma Dispositif de traitement acoustique du bruit emis par un turboreacteur
ES2834442T3 (es) 2011-05-11 2021-06-17 Silentium Ltd Sistema y método de control del ruido
US9928824B2 (en) 2011-05-11 2018-03-27 Silentium Ltd. Apparatus, system and method of controlling noise within a noise-controlled volume
JP5782833B2 (ja) * 2011-05-26 2015-09-24 株式会社Ihi ファン騒音低減装置
DE102012003902A1 (de) * 2011-12-14 2013-06-20 Istvan Bolgar Einlauf für eine Gasturbine
US10036316B2 (en) * 2012-10-02 2018-07-31 United Technologies Corporation Geared turbofan engine with high compressor exit temperature
CN103835810B (zh) * 2012-11-27 2017-02-08 中航商用航空发动机有限责任公司 一种航空发动机进气短舱的声衬装置及航空发动机
FR2999711B1 (fr) * 2012-12-13 2015-07-03 Snecma Methode et dispositif de detection acoustique d'un dysfonctionnement d'un moteur equipe d'un controle actif du bruit.
US9920653B2 (en) 2012-12-20 2018-03-20 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US9932933B2 (en) 2012-12-20 2018-04-03 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
WO2014163673A2 (en) 2013-03-11 2014-10-09 Bronwyn Power Gas turbine engine flow path geometry
EP2971658B1 (de) * 2013-03-13 2022-11-30 Raytheon Technologies Corporation Geräuscharmer verdichter für getriebefan-gasturbinentriebwerk
WO2014197035A2 (en) * 2013-03-15 2014-12-11 United Technologies Corporation Acoustic liner with varied properties
US10156206B2 (en) * 2013-10-24 2018-12-18 United Technologies Corporation Pivoting blocker door
US9919500B2 (en) 2014-09-29 2018-03-20 Pratt & Whitney Canada Corp. Inner bypass duct
KR20170097153A (ko) 2014-12-19 2017-08-25 제네럴 일렉트릭 컴퍼니 능동 소음 제어 시스템
US10371173B2 (en) * 2015-05-07 2019-08-06 United Technologies Corporation Liner for a gas turbine engine
NZ737183A (en) * 2015-05-25 2024-01-26 Dotterel Tech Limited A shroud for an aircraft
US10460717B2 (en) * 2015-12-18 2019-10-29 Amazon Technologies, Inc. Carbon nanotube transducers on propeller blades for sound control
US10344711B2 (en) * 2016-01-11 2019-07-09 Rolls-Royce Corporation System and method of alleviating blade flutter
WO2017183999A1 (en) 2016-04-20 2017-10-26 General Electric Company Active noise cancelation systems and devices
US10458426B2 (en) 2016-09-15 2019-10-29 General Electric Company Aircraft fan with low part-span solidity
US10677264B2 (en) * 2016-10-14 2020-06-09 General Electric Company Supersonic single-stage turbofan engine
AU2018306554A1 (en) 2017-07-24 2020-02-20 Dotterel Technologies Limited Shroud
FR3069850B1 (fr) * 2017-08-01 2019-11-22 Safran Aircraft Engines Systeme actif generant des interferences acoustiques destructives pour moteur d'aeronef a plusieurs corps de soufflante
US10465539B2 (en) * 2017-08-04 2019-11-05 Pratt & Whitney Canada Corp. Rotor casing
JP6689241B2 (ja) 2017-09-15 2020-04-28 株式会社東芝 騒音低減装置、飛行体、発電装置、騒音低減方法及び騒音低減プログラム
US10319360B1 (en) * 2018-03-06 2019-06-11 GM Global Technology Operations LLC Active masking of tonal noise using motor-based acoustic generator to improve sound quality
FR3078744B1 (fr) * 2018-03-08 2020-11-20 Safran Nacelles Dispositif actif d’attenuation des emissions acoustiques pour un turboreacteur comportant des turbines controlees
JP6783813B2 (ja) 2018-03-15 2020-11-11 株式会社東芝 騒音低減装置およびジェットファン
JP6822999B2 (ja) 2018-03-20 2021-01-27 株式会社東芝 動翼騒音低減システム、飛行体、騒音低減システム
JP6826067B2 (ja) 2018-03-20 2021-02-03 株式会社東芝 動翼静翼干渉騒音低減システムおよび飛行体
IL258943A (en) * 2018-04-25 2018-06-03 Technion Res & Development Found Ltd Spatially global noise cancellation
US11163302B2 (en) 2018-09-06 2021-11-02 Amazon Technologies, Inc. Aerial vehicle propellers having variable force-torque ratios
US10900414B2 (en) * 2018-11-23 2021-01-26 Pratt & Whitney Canada Corp. Fan assembly having flow recirculation circuit with guide vanes
JP7039512B2 (ja) 2019-03-12 2022-03-22 株式会社東芝 動翼静翼干渉騒音低減システムおよび飛行体
WO2020202174A1 (en) * 2019-04-01 2020-10-08 Dasari Dileep Systems and methods for increasing the efficiency of axial ducted fans
US11199437B2 (en) * 2019-04-19 2021-12-14 Purdue Research Foundation Utilization of fast-response pressure measurements to nonintrusively monitor blade vibration in axial compressors
FR3103953B1 (fr) * 2019-11-29 2021-11-12 Safran Aircraft Engines Pastille résonante et cellule de traitement acoustique dotée d’une telle pastille
US11747236B2 (en) 2020-09-10 2023-09-05 Virginia Tech Intellectual Properties, Inc. Flow measurement for a gas turbine engine
GB202014210D0 (en) 2020-09-10 2020-10-28 Rolls Royce Plc Gas turbine engine with airflow measurement system
US11821771B2 (en) 2020-09-10 2023-11-21 Virginia Tech Intellectual Properties, Inc. Flow measurement for a gas turbine engine
US11796358B2 (en) 2020-09-10 2023-10-24 Virginia Tech Intellectual Properties, Inc. Flow measurement for a gas turbine engine

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3936606A (en) * 1971-12-07 1976-02-03 Wanke Ronald L Acoustic abatement method and apparatus
US4044203A (en) * 1972-11-24 1977-08-23 National Research Development Corporation Active control of sound waves
FR2370170A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
FR2370171A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
US4421811A (en) * 1979-12-21 1983-12-20 Rohr Industries, Inc. Method of manufacturing double layer attenuation panel with two layers of linear type material
US4452335A (en) * 1982-05-03 1984-06-05 United Technologies Corporation Sound absorbing structure for a gas turbine engine
GB2126837B (en) * 1982-08-19 1986-07-23 British Aerospace Noise suppression
GB8317086D0 (en) * 1983-06-23 1983-07-27 Swinbanks M A Attenuation of sound waves
GB8405914D0 (en) * 1984-03-07 1984-04-11 Swinbanks M A Reducing noise by cancellation
US4689821A (en) * 1985-09-23 1987-08-25 Lockheed Corporation Active noise control system
GB8615315D0 (en) * 1986-06-23 1986-07-30 Secr Defence Aircraft cabin noise control apparatus
DE3735421A1 (de) * 1987-10-20 1989-05-11 Deutsche Forsch Luft Raumfahrt Verfahren zur minderung des ueberfluggeraeusches von flugzeugen mit einem von einem kolbenmotor getriebenen propeller
US4815139A (en) * 1988-03-16 1989-03-21 Nelson Industries, Inc. Active acoustic attenuation system for higher order mode non-uniform sound field in a duct
GB2237415A (en) * 1989-10-20 1991-05-01 Fokker Bv Propeller blade synchrophasing
US5146505A (en) * 1990-10-04 1992-09-08 General Motors Corporation Method for actively attenuating engine generated noise
US5169288A (en) * 1991-09-06 1992-12-08 General Electric Company Low noise fan assembly
US5347586A (en) * 1992-04-28 1994-09-13 Westinghouse Electric Corporation Adaptive system for controlling noise generated by or emanating from a primary noise source
US5386689A (en) * 1992-10-13 1995-02-07 Noises Off, Inc. Active gas turbine (jet) engine noise suppression
US5355417A (en) * 1992-10-21 1994-10-11 The Center For Innovative Technology Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors
US5420383A (en) * 1993-10-22 1995-05-30 United Technologies Corporation Anti-sound arrangement for multi-stage blade cascade
US5382134A (en) * 1993-11-01 1995-01-17 General Electric Company Active noise control using noise source having adaptive resonant frequency tuning through stiffness variation

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EP0715066A2 (de) 1996-06-05
EP0715066A3 (de) 1999-03-03
US5478199A (en) 1995-12-26
DE69524551T2 (de) 2002-08-29
EP0715066B1 (de) 2001-12-12

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