AU2003224839A1 - A catalytic combustion system and method of operating a gas turbine incorporating such a system - Google Patents

A catalytic combustion system and method of operating a gas turbine incorporating such a system

Info

Publication number
AU2003224839A1
AU2003224839A1 AU2003224839A AU2003224839A AU2003224839A1 AU 2003224839 A1 AU2003224839 A1 AU 2003224839A1 AU 2003224839 A AU2003224839 A AU 2003224839A AU 2003224839 A AU2003224839 A AU 2003224839A AU 2003224839 A1 AU2003224839 A1 AU 2003224839A1
Authority
AU
Australia
Prior art keywords
operating
gas turbine
catalytic combustion
turbine incorporating
combustion 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.)
Abandoned
Application number
AU2003224839A
Inventor
Shahram Farhangi
David R. Matthews
Michael P. Moriarty
Kenneth M. Sprouse
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.)
Boeing Co
Original Assignee
Boeing 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
Priority claimed from US10/120,268 external-priority patent/US20030192318A1/en
Priority claimed from US10/189,711 external-priority patent/US20040003598A1/en
Priority claimed from US10/397,394 external-priority patent/US20030192319A1/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of AU2003224839A1 publication Critical patent/AU2003224839A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
AU2003224839A 2002-04-10 2003-04-04 A catalytic combustion system and method of operating a gas turbine incorporating such a system Abandoned AU2003224839A1 (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US10/120,268 2002-04-10
US10/120,268 US20030192318A1 (en) 2002-04-10 2002-04-10 Catalytic combustor for substantially eliminating nitrous oxide emissions
US10/189,711 2002-07-03
US10/189,711 US20040003598A1 (en) 2002-07-03 2002-07-03 Injector apparatus and method for combusting a fuel for a gas powered turbine
US10/397,394 US20030192319A1 (en) 2002-04-10 2003-03-26 Catalytic combustor and method for substantially eliminating nitrous oxide emissions
US10/397,394 2003-03-26
PCT/US2003/010365 WO2003087672A1 (en) 2002-04-10 2003-04-04 A catalytic combustion system and method of operating a gas turbine incorporating such a system

Publications (1)

Publication Number Publication Date
AU2003224839A1 true AU2003224839A1 (en) 2003-10-27

Family

ID=29255199

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003224839A Abandoned AU2003224839A1 (en) 2002-04-10 2003-04-04 A catalytic combustion system and method of operating a gas turbine incorporating such a system

Country Status (3)

Country Link
AU (1) AU2003224839A1 (en)
DE (1) DE10392526B4 (en)
WO (1) WO2003087672A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7117674B2 (en) 2002-04-10 2006-10-10 The Boeing Company Catalytic combustor and method for substantially eliminating various emissions

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59107119A (en) * 1982-12-10 1984-06-21 Toshiba Corp Combustion of gas turbine
JPS6064131A (en) * 1983-09-19 1985-04-12 Toshiba Corp Catalytic burner combustor
JPS6066022A (en) * 1983-09-21 1985-04-16 Toshiba Corp Combustion in gas turbine
DE3474714D1 (en) * 1983-12-07 1988-11-24 Toshiba Kk Nitrogen oxides decreasing combustion method
US4870824A (en) * 1987-08-24 1989-10-03 Westinghouse Electric Corp. Passively cooled catalytic combustor for a stationary combustion turbine
US5461864A (en) * 1993-12-10 1995-10-31 Catalytica, Inc. Cooled support structure for a catalyst
DE19727730A1 (en) * 1997-06-30 1999-01-07 Abb Research Ltd Gas turbine construction
US6415608B1 (en) * 2000-09-26 2002-07-09 Siemens Westinghouse Power Corporation Piloted rich-catalytic lean-burn hybrid combustor
US20020139119A1 (en) * 2001-04-02 2002-10-03 Touchton George L. Combustor with inlet temperature control
US6588213B2 (en) * 2001-09-27 2003-07-08 Siemens Westinghouse Power Corporation Cross flow cooled catalytic reactor for a gas turbine

Also Published As

Publication number Publication date
WO2003087672A1 (en) 2003-10-23
DE10392526B4 (en) 2010-08-12
DE10392526T5 (en) 2005-05-25

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase