JP2012149639A5 - - Google Patents

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Publication number
JP2012149639A5
JP2012149639A5 JP2012002659A JP2012002659A JP2012149639A5 JP 2012149639 A5 JP2012149639 A5 JP 2012149639A5 JP 2012002659 A JP2012002659 A JP 2012002659A JP 2012002659 A JP2012002659 A JP 2012002659A JP 2012149639 A5 JP2012149639 A5 JP 2012149639A5
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JP
Japan
Prior art keywords
stage
exhaust gas
power generation
turbine
generation system
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
JP2012002659A
Other languages
English (en)
Japanese (ja)
Other versions
JP2012149639A (ja
JP5555724B2 (ja
Filing date
Publication date
Priority claimed from US13/007,191 external-priority patent/US8322141B2/en
Application filed filed Critical
Publication of JP2012149639A publication Critical patent/JP2012149639A/ja
Publication of JP2012149639A5 publication Critical patent/JP2012149639A5/ja
Application granted granted Critical
Publication of JP5555724B2 publication Critical patent/JP5555724B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012002659A 2011-01-14 2012-01-11 発電システム Expired - Fee Related JP5555724B2 (ja)

Applications Claiming Priority (2)

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

Publications (3)

Publication Number Publication Date
JP2012149639A JP2012149639A (ja) 2012-08-09
JP2012149639A5 true JP2012149639A5 (enExample) 2013-05-16
JP5555724B2 JP5555724B2 (ja) 2014-07-23

Family

ID=46397773

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012002659A Expired - Fee Related JP5555724B2 (ja) 2011-01-14 2012-01-11 発電システム

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

Family Cites Families (25)

* 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
US4271664A (en) * 1977-07-21 1981-06-09 Hydragon Corporation Turbine engine with exhaust gas recirculation
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
US6622470B2 (en) * 2000-05-12 2003-09-23 Clean Energy Systems, Inc. Semi-closed brayton cycle gas turbine power systems
US6647707B2 (en) * 2000-09-05 2003-11-18 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
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
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

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