| 发明名称 |
GAS TURBINE BRAKING APPARATUS AND METHOD |
| 摘要 |
A device is provided which can serve one or more of the multiple functions of impeding rotation of a shaft de-coupled turbine rotor, selectively impeding rotation of a first spool of the engine, for example to permit a second spool to generate power for use in ground operation, and facilitating reduced aircraft ground speed. |
| 申请公布号 |
CA2577832(A1) |
申请公布日期 |
2006.03.02 |
| 申请号 |
CA20052577832 |
申请日期 |
2005.08.18 |
| 申请人 |
PRATT & WHITNEY CANADA, INC. |
发明人 |
DOOLEY, KEVIN ALLAN;ANDERSON, STEPHEN ARTHUR;BRAND, JOSEPH H.;TRUMPER, RONALD F. |
| 分类号 |
F01D21/00;F01D21/04;F02C7/00;F02C7/36;F16D59/00 |
主分类号 |
F01D21/00 |
| 代理机构 |
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