发明名称 |
FUEL INJECTION LOCATIONS BASED ON COMBUSTOR FLOW PATH |
摘要 |
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. |
申请公布号 |
WO2017002075(A3) |
申请公布日期 |
2017.02.23 |
申请号 |
WO2016IB53943 |
申请日期 |
2016.06.30 |
申请人 |
ANSALDO ENERGIA IP UK LIMITED |
发明人 |
MCNALLY, Joshua R.;PENNEL, Douglas;GAUTHIER, Donald;MATYS, Pawel;PASKIN, Marc;RUCK, Thomas R.;STUTTAFORD, Peter John;SAM, Bernard Tam-Yen;JORGENSEN, Stephen W. |
分类号 |
F23R3/16;F23R3/14;F23R3/20;F23R3/28;F23R3/34;F23R3/44;F23R3/54 |
主分类号 |
F23R3/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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