发明名称 |
RADIAL PRE-SWIRL ASSEMBLY AND COOLING FLUID METERING STRUCTURE FOR A GAS TURBINE ENGINE |
摘要 |
A gas turbine engine comprises a pre-swirl structure coupled to a shaft cover structure and located radially between a supply of cooling fluid and a flow path. The pre-swirl structure defines a flow passage and includes a plurality of swirl members in the flow passage. A flow direction of cooling fluid passing through the flow passage is altered by the swirl members such that the cooling fluid has a velocity component in a direction tangential to the circumferential direction. The bypass passages provide cooling fluid into a turbine rim cavity associated with a first row vane assembly to prevent hot gas ingestion into the turbine rim cavity from a hot gas flow path associated with a turbine section of the engine.
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申请公布号 |
US2011250057(A1) |
申请公布日期 |
2011.10.13 |
申请号 |
US20100859948 |
申请日期 |
2010.08.20 |
申请人 |
LAURELLO VINCENT P;KIMMEL KEITH D;EBERT TODD |
发明人 |
LAURELLO VINCENT P.;KIMMEL KEITH D.;EBERT TODD |
分类号 |
F01D5/08 |
主分类号 |
F01D5/08 |
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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