CH707576A8 - System und Verfahren zur Reduktion des Gegendrucks in einem Gasturbinensystem. - Google Patents

System und Verfahren zur Reduktion des Gegendrucks in einem Gasturbinensystem.

Info

Publication number
CH707576A8
CH707576A8 CH00140/14A CH1402014A CH707576A8 CH 707576 A8 CH707576 A8 CH 707576A8 CH 00140/14 A CH00140/14 A CH 00140/14A CH 1402014 A CH1402014 A CH 1402014A CH 707576 A8 CH707576 A8 CH 707576A8
Authority
CH
Switzerland
Prior art keywords
gas turbine
reducing backpressure
exhaust passage
air
turbine system
Prior art date
Application number
CH00140/14A
Other languages
English (en)
Other versions
CH707576A2 (de
Inventor
Wenjie Wu
Hua Zhang
Brad Aaron Kippel
Yongjiang Hao
Jianmin Zhang
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH707576A2 publication Critical patent/CH707576A2/de
Publication of CH707576A8 publication Critical patent/CH707576A8/de

Links

Classifications

    • 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
    • F01D25/305—Exhaust heads, chambers, or the like with fluid, e.g. liquid injection
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/11—Two-dimensional triangular
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/184—Two-dimensional patterned sinusoidal
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/601—Fluid transfer using an ejector or a jet pump

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

Erfindungsgemäss gehören zu einem System: ein Abgaskanal (17), der dazu eingerichtet ist, einen Abgasstrom zu kanalisieren, und ein Lufteinspeisungssystem (12), das mit dem Abgaskanal (17) verbunden ist, wobei das Lufteinspeisungssystem (12) einen ersten Luftinjektor (13) enthält, der dazu eingerichtet ist, in den Abgaskanal Luft einzuspeisen, um den Strom des Abgases durch den Abgaskanal (17) zu fördern.
CH00140/14A 2013-02-15 2014-02-03 System und Verfahren zur Reduktion des Gegendrucks in einem Gasturbinensystem. CH707576A8 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320089712.6U CN203441604U (zh) 2013-02-15 2013-02-15 用于降低燃气涡轮系统中的背压的系统

Publications (2)

Publication Number Publication Date
CH707576A2 CH707576A2 (de) 2014-08-15
CH707576A8 true CH707576A8 (de) 2014-10-15

Family

ID=50092663

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00140/14A CH707576A8 (de) 2013-02-15 2014-02-03 System und Verfahren zur Reduktion des Gegendrucks in einem Gasturbinensystem.

Country Status (5)

Country Link
US (1) US9644498B2 (de)
JP (1) JP2014167293A (de)
CN (1) CN203441604U (de)
CH (1) CH707576A8 (de)
DE (1) DE102014101147A1 (de)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2896793B1 (de) * 2014-01-21 2024-08-28 Ansaldo Energia Switzerland AG Verfahren zum Betrieb einer Gasturbinenanordnung und die Gasturbinenanordnung
GB201420966D0 (en) * 2014-11-26 2015-01-07 Rolls Royce Plc Compressor cooling
US10731560B2 (en) 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
US10100739B2 (en) 2015-05-18 2018-10-16 United Technologies Corporation Cooled cooling air system for a gas turbine engine
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US20160376908A1 (en) * 2015-06-29 2016-12-29 General Electric Company Power generation system exhaust cooling
US9752503B2 (en) * 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US9752502B2 (en) 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US10060316B2 (en) 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) * 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US10215070B2 (en) 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
US10794288B2 (en) 2015-07-07 2020-10-06 Raytheon Technologies Corporation Cooled cooling air system for a turbofan engine
US10267185B2 (en) * 2015-07-30 2019-04-23 General Electric Company System and method for controlling coolant supply to an exhaust gas
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
US9976479B2 (en) * 2015-12-15 2018-05-22 General Electric Company Power plant including a static mixer and steam generating system via turbine extraction and compressor extraction
US9970354B2 (en) * 2015-12-15 2018-05-15 General Electric Company Power plant including an ejector and steam generating system via turbine extraction and compressor extraction
US9964035B2 (en) * 2015-12-15 2018-05-08 General Electric Company Power plant including exhaust gas coolant injection system and steam generating system via turbine extraction
US9890710B2 (en) * 2015-12-15 2018-02-13 General Electric Company Power plant with steam generation via combustor gas extraction
US10072573B2 (en) * 2015-12-15 2018-09-11 General Electric Company Power plant including an ejector and steam generating system via turbine extraction
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling
US10669940B2 (en) 2016-09-19 2020-06-02 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and turbine drive
IT201600107332A1 (it) * 2016-10-25 2018-04-25 Nuovo Pignone Tecnologie Srl Sistema di turbina a gas con disposizione per convogliare lo spurgo / gas turbine system with bleed routing arrangement
US10794290B2 (en) 2016-11-08 2020-10-06 Raytheon Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10550768B2 (en) 2016-11-08 2020-02-04 United Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10961911B2 (en) 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
EP3354867A1 (de) * 2017-01-27 2018-08-01 Siemens Aktiengesellschaft Abgasleitung für einen mit fossilem brennstoff angetriebenen motor eines systems zur selektiven katalytischen reduktion mit verdünnung
US10577964B2 (en) 2017-03-31 2020-03-03 United Technologies Corporation Cooled cooling air for blade air seal through outer chamber
US10711640B2 (en) 2017-04-11 2020-07-14 Raytheon Technologies Corporation Cooled cooling air to blade outer air seal passing through a static vane
EP3460210B1 (de) * 2017-09-25 2020-07-15 General Electric Technology GmbH Temperiersystem für selektives gasturbinenkatalysatorreduzierungssystem
US11788466B2 (en) * 2017-12-08 2023-10-17 Schlumberger Technology Corporation Compressed N2 for energy storage
US11725584B2 (en) * 2018-01-17 2023-08-15 General Electric Company Heat engine with heat exchanger
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
FR3110197B1 (fr) * 2020-05-14 2022-12-23 Ge Energy Products France Snc Systeme de purge d’un combustible au gaz reactif
US11788470B2 (en) 2021-03-01 2023-10-17 General Electric Company Gas turbine engine thermal management
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly
US12410752B2 (en) 2021-09-23 2025-09-09 General Electric Company System and method of detecting an airflow fault condition
US11702958B2 (en) 2021-09-23 2023-07-18 General Electric Company System and method of regulating thermal transport bus pressure
US12410753B2 (en) 2022-11-01 2025-09-09 General Electric Company Gas turbine engine
US12428992B2 (en) 2022-11-01 2025-09-30 General Electric Company Gas turbine engine
US12503980B2 (en) 2022-11-01 2025-12-23 General Electric Company Gas turbine engine
US12196131B2 (en) 2022-11-01 2025-01-14 General Electric Company Gas turbine engine
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine
US12535033B2 (en) 2022-11-01 2026-01-27 General Electric Company Gas turbine engine
US12540551B1 (en) 2025-07-01 2026-02-03 General Electric Company Gas turbine engines including splittered airfoils

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4146986A (en) * 1975-12-25 1979-04-03 Nippon Soken, Inc. Device for supplying secondary air for purifying exhaust gases discharged from internal combustion engine
US4171112A (en) * 1977-07-29 1979-10-16 Rolls-Royce Limited V.S.T.O.L. aircraft with control means for maintaining substantially equal thrust on both sides of the aircraft
US4215536A (en) * 1978-12-26 1980-08-05 The Boeing Company Gas turbine mixer apparatus
US5340271A (en) * 1990-08-18 1994-08-23 Rolls-Royce Plc Flow control method and means
US5414992A (en) * 1993-08-06 1995-05-16 United Technologies Corporation Aircraft cooling method
US5787707A (en) * 1994-08-02 1998-08-04 Corning Incorporated In-line adsorber system
JPH08218844A (ja) * 1995-02-07 1996-08-27 Hiromi Mochida 自動車の排気ガス熱の回収装置
US5934069A (en) * 1995-06-08 1999-08-10 Corning Incorporated In-line adsorber system
US5974802A (en) 1997-01-27 1999-11-02 Alliedsignal Inc. Exhaust gas recirculation system employing a fluidic pump
JP2001317327A (ja) * 2000-05-11 2001-11-16 Tokai Clean Kaihatsu:Kk 微粒子除去装置
US6336319B1 (en) * 2000-05-26 2002-01-08 General Electric Company Fluidic nozzle control system
US6622472B2 (en) * 2001-10-17 2003-09-23 Gateway Space Transport, Inc. Apparatus and method for thrust vector control
US7069716B1 (en) * 2002-04-24 2006-07-04 Express Integrated Technologies Llc Cooling air distribution apparatus
US6896475B2 (en) * 2002-11-13 2005-05-24 General Electric Company Fluidic actuation for improved diffuser performance
US7137245B2 (en) * 2004-06-18 2006-11-21 General Electric Company High area-ratio inter-turbine duct with inlet blowing
ES2818028T3 (es) 2004-12-20 2021-04-09 Antibodyshop As Determinación de lipocalina asociada a gelatinasa de neutrófilos (NGAL) como marcador diagnóstico para trastornos renales
US7509797B2 (en) * 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
US7549282B2 (en) 2005-10-25 2009-06-23 General Electric Company Multi-slot inter-turbine duct assembly for use in a turbine engine
US7536864B2 (en) * 2005-12-07 2009-05-26 General Electric Company Variable motive nozzle ejector for use with turbine engines
GB2451261B (en) 2007-07-25 2011-08-24 Anthony Gregory Smith Gas turbine engine nozzle
JP5293941B2 (ja) * 2008-06-11 2013-09-18 株式会社Ｉｈｉ 集塵フィルタの再生方法
CN201241751Y (zh) 2008-08-12 2009-05-20 路兴荣 发动机进气增压装置
US20100205967A1 (en) 2009-02-16 2010-08-19 General Electric Company Pre-heating gas turbine inlet air using an external fired heater and reducing overboard bleed in low-btu applications
US8668449B2 (en) * 2009-06-02 2014-03-11 Siemens Energy, Inc. Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow
US8647057B2 (en) 2009-06-02 2014-02-11 Siemens Energy, Inc. Turbine exhaust diffuser with a gas jet producing a coanda effect flow control
US8516786B2 (en) * 2009-08-13 2013-08-27 General Electric Company System and method for injection of cooling air into exhaust gas flow
US20120186261A1 (en) * 2011-01-20 2012-07-26 General Electric Company System and method for a gas turbine exhaust diffuser
JP5571015B2 (ja) * 2011-02-25 2014-08-13 三菱重工業株式会社 ガスタービン
US8556027B2 (en) * 2011-06-28 2013-10-15 United Technologies Corporation Eductor exhaust silencer assembly with bypass gasflow
US8430202B1 (en) * 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
EP2857656A1 (de) * 2013-10-01 2015-04-08 Alstom Technology Ltd Gasturbine mit Kühlluftkühlsystem und Verfahren zum Betrieb einer Gasturbine bei niedriger Teillast

Also Published As

Publication number Publication date
US20140230444A1 (en) 2014-08-21
US9644498B2 (en) 2017-05-09
CN203441604U (zh) 2014-02-19
CH707576A2 (de) 2014-08-15
DE102014101147A1 (de) 2014-08-21
JP2014167293A (ja) 2014-09-11

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