| 发明名称 |
START SYSTEM FOR GAS TURBINE ENGINES |
| 摘要 |
A gas turbine engine includes a flow control mechanism operable to direct at least a portion of a fan airflow from a secondary flow path into a core flow path.
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| 申请公布号 |
US2013183136(A1) |
申请公布日期 |
2013.07.18 |
| 申请号 |
US201213352296 |
申请日期 |
2012.01.17 |
| 申请人 |
ROBERGE GARY D.;BERRYANN ANDREW P.;CARR SCOTT A. |
发明人 |
ROBERGE GARY D.;BERRYANN ANDREW P.;CARR SCOTT A. |
| 分类号 |
F01D1/04;F01D25/24 |
主分类号 |
F01D1/04 |
| 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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