Title:
FUEL INJECTION LOCATIONS BASED ON COMBUSTOR FLOW PATH
Document Type and Number:
WIPO Patent Application WO/2017/002075
Kind Code:
A3
Abstract:
Systems and methods for dual-fuel operation of a gas turbine combustor are provided. An exemplary gas turbine combustor may comprise one or more components, such as a cylindrical combustion liner, a flow sleeve, a main mixer, a radial inflow swirler, a combustor dome, and a fuel cartridge assembly, one or more of which may be configured to supply either a gaseous or a liquid fuel to the combustion liner, depending on whether gaseous fuel operation or liquid fuel operation of the combustor is desired.
Inventors:
MCNALLY JOSHUA R (US)
PENNEL DOUGLAS (CH)
GAUTHIER DONALD (US)
MATYS PAWEL (US)
PASKIN MARC (US)
RUCK THOMAS R (CH)
STUTTAFORD PETER JOHN (US)
SAM BERNARD TAM-YEN (US)
JORGENSEN STEPHEN W (US)
PENNEL DOUGLAS (CH)
GAUTHIER DONALD (US)
MATYS PAWEL (US)
PASKIN MARC (US)
RUCK THOMAS R (CH)
STUTTAFORD PETER JOHN (US)
SAM BERNARD TAM-YEN (US)
JORGENSEN STEPHEN W (US)
Application Number:
PCT/IB2016/053943
Publication Date:
February 23, 2017
Filing Date:
June 30, 2016
Export Citation:
Assignee:
ANSALDO ENERGIA IP UK LTD (GB)
International Classes:
F23R3/14; F23R3/16; F23R3/20; F23R3/28; F23R3/34; F23R3/44; F23R3/54
Domestic Patent References:
| WO2014055437A1 | 2014-04-10 |
Foreign References:
| US20060168966A1 | 2006-08-03 | |||
| US7137256B1 | 2006-11-21 | |||
| US20130098040A1 | 2013-04-25 |
Attorney, Agent or Firm:
BERNOTTI, Andrea et al. (IT)
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