CN102588110B - 功率生成系统 - Google Patents

功率生成系统 Download PDF

Info

Publication number
CN102588110B
CN102588110B CN201210028067.7A CN201210028067A CN102588110B CN 102588110 B CN102588110 B CN 102588110B CN 201210028067 A CN201210028067 A CN 201210028067A CN 102588110 B CN102588110 B CN 102588110B
Authority
CN
China
Prior art keywords
order
exhaust gas
power generation
generation system
burner
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
CN201210028067.7A
Other languages
English (en)
Chinese (zh)
Other versions
CN102588110A (zh
Inventor
J·C·因泰尔
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 CN102588110A publication Critical patent/CN102588110A/zh
Application granted granted Critical
Publication of CN102588110B publication Critical patent/CN102588110B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/56—Combustion chambers having rotary flame tubes
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201210028067.7A 2011-01-14 2012-01-13 功率生成系统 Expired - Fee Related CN102588110B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/007,191 US8322141B2 (en) 2011-01-14 2011-01-14 Power generation system including afirst turbine stage structurally incorporating a combustor
US13/007,191 2011-01-14
US13/007191 2011-01-14

Publications (2)

Publication Number Publication Date
CN102588110A CN102588110A (zh) 2012-07-18
CN102588110B true CN102588110B (zh) 2016-05-18

Family

ID=46397773

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210028067.7A Expired - Fee Related CN102588110B (zh) 2011-01-14 2012-01-13 功率生成系统

Country Status (5)

Country Link
US (1) US8322141B2 (enExample)
JP (1) JP5555724B2 (enExample)
CN (1) CN102588110B (enExample)
DE (1) DE102012100273A1 (enExample)
FR (1) FR2970511B1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI127654B (en) 2014-05-21 2018-11-30 Finno Energy Oy System and method for generating electrical energy
US10107498B2 (en) * 2014-12-11 2018-10-23 General Electric Company Injection systems for fuel and gas
CN105298645A (zh) * 2015-09-18 2016-02-03 中国航空工业集团公司沈阳发动机设计研究所 一种外涵回热燃气轮机循环系统

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4271664A (en) * 1977-07-21 1981-06-09 Hydragon Corporation Turbine engine with exhaust gas recirculation
CN101029599A (zh) * 2006-02-21 2007-09-05 通用电气公司 组装燃气涡轮发动机的方法和设备

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3309866A (en) * 1965-03-11 1967-03-21 Gen Electric Combustion process and apparatus
US5003766A (en) * 1984-10-10 1991-04-02 Paul Marius A Gas turbine engine
JP2820558B2 (ja) * 1991-10-22 1998-11-05 三菱重工業株式会社 燃焼器とタービン静翼一体型ガスタービン
US5881549A (en) * 1993-10-19 1999-03-16 California Energy Commission Reheat enhanced gas turbine powerplants
US5535584A (en) * 1993-10-19 1996-07-16 California Energy Commission Performance enhanced gas turbine powerplants
US5490377A (en) * 1993-10-19 1996-02-13 California Energy Commission Performance enhanced gas turbine powerplants
JP4031590B2 (ja) * 1999-03-08 2008-01-09 三菱重工業株式会社 燃焼器の尾筒シール構造及びその構造を用いたガスタービン
US6378287B2 (en) * 2000-03-17 2002-04-30 Kenneth F. Griffiths Multi-stage turbomachine and design method
US6824710B2 (en) * 2000-05-12 2004-11-30 Clean Energy Systems, Inc. Working fluid compositions for use in semi-closed brayton cycle gas turbine power systems
EP1780387A3 (en) * 2000-09-05 2007-07-18 Sudarshan Paul Dev Nested core gas turbine engine
FR2825785B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Liaison de chambre de combustion cmc de turbomachine en deux parties
WO2002103164A1 (en) * 2001-06-18 2002-12-27 Griffiths Kenneth F Multi-stage turbo-machines with specific blade aspect ratios
US6619026B2 (en) * 2001-08-27 2003-09-16 Siemens Westinghouse Power Corporation Reheat combustor for gas combustion turbine
US6796130B2 (en) * 2002-11-07 2004-09-28 Siemens Westinghouse Power Corporation Integrated combustor and nozzle for a gas turbine combustion system
US7509809B2 (en) * 2005-06-10 2009-03-31 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
US7451600B2 (en) * 2005-07-06 2008-11-18 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
US7784261B2 (en) * 2006-05-25 2010-08-31 Siemens Energy, Inc. Combined cycle power plant
US7603863B2 (en) 2006-06-05 2009-10-20 General Electric Company Secondary fuel injection from stage one nozzle
US20080134685A1 (en) * 2006-12-07 2008-06-12 Ronald Scott Bunker Gas turbine guide vanes with tandem airfoils and fuel injection and method of use
US8006477B2 (en) * 2008-04-01 2011-08-30 General Electric Company Re-heat combustor for a gas turbine engine
US8397482B2 (en) 2008-05-15 2013-03-19 General Electric Company Dry 3-way catalytic reduction of gas turbine NOx
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
US8381525B2 (en) * 2009-09-30 2013-02-26 General Electric Company System and method using low emissions gas turbine cycle with partial air separation

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4271664A (en) * 1977-07-21 1981-06-09 Hydragon Corporation Turbine engine with exhaust gas recirculation
CN101029599A (zh) * 2006-02-21 2007-09-05 通用电气公司 组装燃气涡轮发动机的方法和设备

Also Published As

Publication number Publication date
JP5555724B2 (ja) 2014-07-23
FR2970511B1 (fr) 2016-03-11
DE102012100273A1 (de) 2012-07-19
FR2970511A1 (fr) 2012-07-20
CN102588110A (zh) 2012-07-18
US8322141B2 (en) 2012-12-04
JP2012149639A (ja) 2012-08-09
US20120180499A1 (en) 2012-07-19

Similar Documents

Publication Publication Date Title
US8806849B2 (en) System and method of operating a power generation system with an alternative working fluid
US8863523B2 (en) System for supplying a working fluid to a combustor
US8112999B2 (en) Turbomachine injection nozzle including a coolant delivery system
CN101865470B (zh) 具有内冷却的燃气涡轮机预混合器
US9133722B2 (en) Transition duct with late injection in turbine system
US20100024378A1 (en) System and method of operating a gas turbine engine with an alternative working fluid
US8281601B2 (en) Systems and methods for reintroducing gas turbine combustion bypass flow
US20100024433A1 (en) System and method of operating a gas turbine engine with an alternative working fluid
US20170114717A1 (en) Axial stage combustion system with exhaust gas recirculation
US20080282667A1 (en) Method and apparatus to facilitate cooling turbine engines
CN204026742U (zh) 用于将燃料供应到燃烧器的系统
JP2014115072A (ja) ガス・タービン・エンジンの燃焼器用燃料ノズル
US20170268776A1 (en) Gas turbine flow sleeve mounting
US8745986B2 (en) System and method of supplying fuel to a gas turbine
CN102588110B (zh) 功率生成系统
US20170058769A1 (en) SYSTEM AND METHOD FOR OPERATING A DRY LOW NOx COMBUSTOR IN A NON-PREMIX MODE
US10344978B2 (en) Combustion liner cooling
US20130227928A1 (en) Fuel nozzle assembly for use in turbine engines and method of assembling same
US8720179B2 (en) Power plant including an exhaust gas recirculation system for injecting recirculated exhaust gases in the fuel and compressed air of a gas turbine engine
US8448442B2 (en) Flexible combustor fuel nozzle
JP2013133823A (ja) ガスタービンからの酸素エミッションを制御するシステム及び方法
CN104204680B (zh) 燃烧装置
US20250067213A1 (en) Flash-atomizing ammonia in a gas turbine combustor
US10228135B2 (en) Combustion liner cooling
US20140123623A1 (en) Gas turbomachine system including an inlet chiller condensate recovery system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160518

Termination date: 20180113