发明名称 |
Turbocharger-based bleed-air driven fuel gas booster system and method |
摘要 |
A method and system for increasing the pressure of gaseous fuel delivered to a fuel system of a gas turbine engine. A portion of pressurized gas or compressed air is discharged from a high-pressure section of the gas turbine engine and is communicated to a plurality of radial inflow turbines or axial flow turbines. Energy is transferred from each turbine to a plurality of compressors driven by the turbines. Gaseous fuel is supplied to an inlet of one of the compressors. The compressed gaseous fuel is then cooled downstream of the compressors. The aftercooled and compressed gaseous fuel is delivered to the fuel system of the gas turbine engine.
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申请公布号 |
US5329757(A) |
申请公布日期 |
1994.07.19 |
申请号 |
US19930060410 |
申请日期 |
1993.05.12 |
申请人 |
GAS RESEARCH INSTITUTE |
发明人 |
FAULKNER, HENRY B.;KESSELI, JAMES B.;SWARDEN, MICHAEL C.;JANSEN, WILLEM |
分类号 |
F02B43/00;F02C3/22;F02C6/10;(IPC1-7):F02C3/22 |
主分类号 |
F02B43/00 |
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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