| 发明名称 |
GAS TURBINE ENGINE BUFFER SYSTEM |
| 摘要 |
A gas turbine engine includes a buffer system that includes a first circuit and a second circuit. The first circuit can communicate a first buffer supply air to a first portion of the gas turbine engine and the second circuit can communicate a second buffer supply air to a second portion of the gas turbine engine.
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| 申请公布号 |
US2013192239(A1) |
申请公布日期 |
2013.08.01 |
| 申请号 |
US201213362349 |
申请日期 |
2012.01.31 |
| 申请人 |
GLAHN JORN A.;ACKERMANN WILLIAM K.;CRAWLEY CLIFTON J.;STRIPINIS PHILIP S. |
发明人 |
GLAHN JORN A.;ACKERMANN WILLIAM K.;CRAWLEY CLIFTON J.;STRIPINIS PHILIP S. |
| 分类号 |
F02C7/12;F02C6/08 |
主分类号 |
F02C7/12 |
| 代理机构 |
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代理人 |
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| 主权项 |
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