发明名称 |
GAS TURBINE ENGINE COOLING VALVE |
摘要 |
A cooling system for a gas turbine engine includes a first structure movable relative to a second structure. The first structure has a cavity. A valve selectively controls fluid flow from a cooling source to the cavity. A valve is configured to move between first and second fluid flow positions in response to movement of the first structure. The first fluid flow position provides a greater amount of cooling fluid from the cooling source to the cavity than in the second fluid flow position.
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申请公布号 |
US2013104557(A1) |
申请公布日期 |
2013.05.02 |
申请号 |
US201113284041 |
申请日期 |
2011.10.28 |
申请人 |
MCMAHON SHAWN M.;PARRISH RUSSELL P. |
发明人 |
MCMAHON SHAWN M.;PARRISH RUSSELL P. |
分类号 |
F02C1/00;F28F27/00 |
主分类号 |
F02C1/00 |
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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