发明名称 |
SYSTEM AND METHOD FOR OPERATING A GAS TURBINE ENGINE |
摘要 |
A system includes a gas turbine engine, which includes a compressor configured to generate compressed air and a turbine. The turbine includes a stationary component and a conduit configured to convey the compressed air from the compressor to the stationary component in a forward direction. The gas turbine engine also includes a flow control device coupled to the conduit. The conduit is configured to convey a gas path air from the stationary component in a reverse direction opposite from the forward direction when the flow control device is in a startup mode. The gas turbine engine also includes a shaft coupled to the compressor and the turbine. |
申请公布号 |
US2014072399(A1) |
申请公布日期 |
2014.03.13 |
申请号 |
US201213607619 |
申请日期 |
2012.09.07 |
申请人 |
MALDONADO JAIME JAVIER;DUTTA SANDIP;GENERAL ELECTRIC COMPANY |
发明人 |
MALDONADO JAIME JAVIER;DUTTA SANDIP |
分类号 |
F01D25/10;F01D17/00 |
主分类号 |
F01D25/10 |
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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