发明名称 |
CONTOURED BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE |
摘要 |
A blade outer air seal (BOAS) segment according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face that circumferentially extend between a first mate face and a second mate face and axially extend between a leading edge face and a trailing edge face, wherein a radial position of the radially inner face varies at a given axial position. |
申请公布号 |
US2016003082(A1) |
申请公布日期 |
2016.01.07 |
申请号 |
US201414771281 |
申请日期 |
2014.02.04 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Lutjen Paul M.;Bruskotter Michael J. |
分类号 |
F01D11/12;F01D25/12;F01D9/04 |
主分类号 |
F01D11/12 |
代理机构 |
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代理人 |
|
主权项 |
1. A blade outer air seal (BOAS) segment, comprising:
a seal body having a radially inner face that circumferentially extend between a first mate face and a second mate face and axially extend between a leading edge face and a trailing edge face, wherein a radial position of the radially inner face varies at a given axial position. |
地址 |
Hartford CT US |