CN102155298B - 用于噪声减少的喷射器/混合器喷嘴 - Google Patents

用于噪声减少的喷射器/混合器喷嘴 Download PDF

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Publication number
CN102155298B
CN102155298B CN201110005640.8A CN201110005640A CN102155298B CN 102155298 B CN102155298 B CN 102155298B CN 201110005640 A CN201110005640 A CN 201110005640A CN 102155298 B CN102155298 B CN 102155298B
Authority
CN
China
Prior art keywords
manifold
entrance
discharging
venting
compressor air
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
CN201110005640.8A
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English (en)
Chinese (zh)
Other versions
CN102155298A (zh
Inventor
张华�
D·W·鲍尔
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 CN102155298A publication Critical patent/CN102155298A/zh
Application granted granted Critical
Publication of CN102155298B publication Critical patent/CN102155298B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N1/00—Silencing apparatus characterised by method of silencing
    • F01N1/14—Silencing apparatus characterised by method of silencing by adding air to exhaust gases
    • 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
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/34—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for attenuating noise
    • 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
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • 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
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • 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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
CN201110005640.8A 2010-01-04 2011-01-04 用于噪声减少的喷射器/混合器喷嘴 Expired - Fee Related CN102155298B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/651,585 US8272222B2 (en) 2010-01-04 2010-01-04 Inlet bleed heat system with ejector/mixer nozzles for noise reduction
US12/651585 2010-01-04

Publications (2)

Publication Number Publication Date
CN102155298A CN102155298A (zh) 2011-08-17
CN102155298B true CN102155298B (zh) 2015-11-25

Family

ID=43827840

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110005640.8A Expired - Fee Related CN102155298B (zh) 2010-01-04 2011-01-04 用于噪声减少的喷射器/混合器喷嘴

Country Status (4)

Country Link
US (1) US8272222B2 (https=)
EP (1) EP2354493B1 (https=)
JP (1) JP2011137453A (https=)
CN (1) CN102155298B (https=)

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JP5010499B2 (ja) * 2008-02-28 2012-08-29 三菱重工業株式会社 ガスタービン及びガスタービンの保守点検方法
US8932004B2 (en) * 2011-11-08 2015-01-13 General Electric Company Inlet bleed heat system
US8926265B2 (en) * 2011-11-08 2015-01-06 General Electric Company Inlet bleed heat system
US8844258B2 (en) * 2011-11-23 2014-09-30 General Electric Company Systems and methods for de-icing a gas turbine engine inlet screen and dehumidifying inlet air filters
KR20140142737A (ko) 2012-04-02 2014-12-12 파워페이즈 엘엘씨 가스 터빈 엔진을 위한 압축 공기 분사 시스템 방법 및 장치
JP5984535B2 (ja) * 2012-07-03 2016-09-06 三菱日立パワーシステムズ株式会社 ガスタービンの氷結防止方法
CN109681329B (zh) 2012-10-26 2022-03-22 鲍尔法斯有限责任公司 燃气轮机能量补充系统和加热系统
US9157333B2 (en) * 2012-11-06 2015-10-13 General Electric Company Inlet bleed heat system with integrated air knife/silencer panels
FR2997996B1 (fr) * 2012-11-12 2015-01-09 Snecma Support de tube d'evacuation d'air dans une turbomachine
US9447732B2 (en) * 2012-11-26 2016-09-20 General Electric Company Gas turbine anti-icing system
US9470150B2 (en) 2013-04-30 2016-10-18 General Electric Company Gas turbine power augmentation system
EP2824285B1 (en) * 2013-07-11 2016-03-16 Alstom Technology Ltd Gas turbine engine comprising an inlet flow control arrangement
EP2837794A1 (en) * 2013-08-14 2015-02-18 Alstom Technology Ltd Improved intake arrangement in gas turbine power plant
US9359951B2 (en) * 2013-09-06 2016-06-07 General Electric Company Inlet bleed heat system and related method for a compact gas turbine inlet
US9494050B2 (en) 2013-09-20 2016-11-15 The Boeing Company Concentric nozzles for enhanced mixing of fluids
US10036321B2 (en) * 2014-05-29 2018-07-31 General Electric Company Systems and methods for utilizing gas turbine compartment ventilation discharge air
US9771865B2 (en) 2014-10-28 2017-09-26 General Electric Company Inlet bleed heat manifold including acoustically treated feed pipe
US10066632B2 (en) 2015-12-10 2018-09-04 General Electric Company Inlet bleed heat control system
US10704464B2 (en) 2016-02-16 2020-07-07 General Electric Company Acoustic nozzles for inlet bleed heat systems
US20170292456A1 (en) * 2016-04-12 2017-10-12 General Electric Company Integrated gas turbine inlet silencer and bleed heat system
US10215193B2 (en) 2017-01-31 2019-02-26 Meggitt Aerospace Ltd. Valve assembly
US20180274445A1 (en) * 2017-03-21 2018-09-27 General Electric Company Inlet Bleed Heat Duct Assembly
US10968828B2 (en) * 2019-03-06 2021-04-06 General Electric Company Anti-icing system for a gas turbine
CN110454285A (zh) * 2019-09-06 2019-11-15 烟台杰瑞石油装备技术有限公司 一种涡轮发动机的隔声舱体
US12292067B2 (en) 2019-09-06 2025-05-06 Yantai Jereh Petroleum Equipment & Technologies Co., Ltd. Turbine engine air intake system and cabin
US12540575B2 (en) 2019-09-06 2026-02-03 Yantai Jereh Petroleum Equipment & Technologies Co., Ltd. Hydraulic fracturing system for driving a plunger pump with a turbine engine and noise reduction thereof
US11391207B2 (en) 2020-01-16 2022-07-19 General Electric Company Anti-icing system having a nozzle with a deflector plate and method
US11459951B2 (en) * 2020-12-22 2022-10-04 General Electric Company Anti-icing system with a flow-deflector assembly
US11473501B2 (en) * 2020-12-22 2022-10-18 General Electric Company Anti-icing for gas turbine system
US12565856B2 (en) 2023-08-16 2026-03-03 Ge Infrastructure Technology Llc Anti-icing and bleed heat system for a gas turbine system

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5157916A (en) * 1990-11-02 1992-10-27 United Technologies Corporation Apparatus and method for suppressing sound in a gas turbine engine powerplant
CN1086581A (zh) * 1992-11-03 1994-05-11 程大酉 改进的回热并联复合双流体热机
US5560195A (en) * 1995-02-13 1996-10-01 General Electric Co. Gas turbine inlet heating system using jet blower
US5761900A (en) * 1995-10-11 1998-06-09 Stage Iii Technologies, L.C. Two-stage mixer ejector suppressor
US6082635A (en) * 1996-06-12 2000-07-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Undulated nozzle for enhanced exit area mixing
US6250064B1 (en) * 1999-05-07 2001-06-26 General Electric Co. Gas turbine inlet air integrated water saturation and supersaturation system and related process
CN1582364A (zh) * 2001-11-02 2005-02-16 阿尔斯通技术有限公司 燃气涡轮机组

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JP2877098B2 (ja) * 1995-12-28 1999-03-31 株式会社日立製作所 ガスタービン，コンバインドサイクルプラント及び圧縮機
US6027304A (en) * 1998-05-27 2000-02-22 General Electric Co. High pressure inlet bleed heat system for the compressor of a turbine
US6226974B1 (en) * 1999-06-25 2001-05-08 General Electric Co. Method of operation of industrial gas turbine for optimal performance
JP3713173B2 (ja) * 1999-12-15 2005-11-02 株式会社日立製作所 ガスタービンの氷結防止運転方法
US8136361B2 (en) * 2006-05-04 2012-03-20 General Electric Company Methods and apparatus for assembling a low noise ejector motive nozzle
US7698898B2 (en) * 2007-04-04 2010-04-20 General Electric Company Mixer for cooling and sealing air system for turbomachinery
US8001789B2 (en) * 2008-03-26 2011-08-23 Alstom Technologies Ltd., Llc Utilizing inlet bleed heat to improve mixing and engine turndown

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5157916A (en) * 1990-11-02 1992-10-27 United Technologies Corporation Apparatus and method for suppressing sound in a gas turbine engine powerplant
CN1086581A (zh) * 1992-11-03 1994-05-11 程大酉 改进的回热并联复合双流体热机
US5560195A (en) * 1995-02-13 1996-10-01 General Electric Co. Gas turbine inlet heating system using jet blower
US5761900A (en) * 1995-10-11 1998-06-09 Stage Iii Technologies, L.C. Two-stage mixer ejector suppressor
US6082635A (en) * 1996-06-12 2000-07-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Undulated nozzle for enhanced exit area mixing
US6250064B1 (en) * 1999-05-07 2001-06-26 General Electric Co. Gas turbine inlet air integrated water saturation and supersaturation system and related process
CN1582364A (zh) * 2001-11-02 2005-02-16 阿尔斯通技术有限公司 燃气涡轮机组

Also Published As

Publication number Publication date
CN102155298A (zh) 2011-08-17
EP2354493B1 (en) 2018-04-11
JP2011137453A (ja) 2011-07-14
EP2354493A3 (en) 2016-12-14
US20110162383A1 (en) 2011-07-07
US8272222B2 (en) 2012-09-25
EP2354493A2 (en) 2011-08-10

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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20151125

Termination date: 20200104