Title:
HYBRID LEAN PREMIXING CATALYTIC COMBUSTION SYSTEM FOR GAS TURBINES
Document Type and Number:
WIPO Patent Application WO2003067054
Kind Code:
A3
Abstract:
A system and method of combusting a hydrocarbon fuel is disclosed. The system comprises air stage valve (54), fuel-air mixing section (61), catalyst section (60), combustor (65) and bypass manifold (57).
More Like This:
JP2011112030 | GAS SUPPLY DEVICE AND EXHAUST GAS POWER GENERATION SYSTEM |
WO/2014/109788 | GAS GENERATOR WITH MOUNT HAVING AIR PASSAGES |
JP5751982 | Power plant and its remodeling method |
Inventors:
CRITCHLEY IAN L
Application Number:
PCT/US2003/000900
Publication Date:
November 20, 2003
Filing Date:
January 13, 2003
Export Citation:
Assignee:
VERICOR POWER SYSTEMS LLC (US)
International Classes:
F02C9/16; F23R3/26; F23R3/34; F23R3/40; (IPC1-7): F02C7/22
Foreign References:
US3975900A | 1976-08-24 | |||
US3121526A | 1964-02-18 | |||
US6098396A | 2000-08-08 | |||
US4285193A | 1981-08-25 |
Download PDF:
Previous Patent: AIR TURBINE STARTER WITH FLUID FLOW CONTROL
Next Patent: METHOD FOR OPERATING A GAS TURBINE HAVING SEVERAL BURNERS
Next Patent: METHOD FOR OPERATING A GAS TURBINE HAVING SEVERAL BURNERS