| 发明名称 |
TURBINE SHROUD THERMAL DISTORTION CONTROL |
| 摘要 |
A shroud for a gas turbine engine includes a leading portion having a leading edge and a first set of circumferentially spaced slots at the leading edge that break up the leading portion into circumferentially spaced segments separated by the first set of slots, and a trailing portion adjacent to the leading portion. The trailing portion has a trailing edge. |
| 申请公布号 |
US2013094946(A1) |
申请公布日期 |
2013.04.18 |
| 申请号 |
US201213668733 |
申请日期 |
2012.11.05 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION;UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHI JUN;GREEN KEVIN E.;BUTLER SHAOLUO L.;SRINIVASAN GAJAWALLI V.;LEVASSEUR GLENN N. |
| 分类号 |
F01D11/18 |
主分类号 |
F01D11/18 |
| 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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