发明名称 |
SEAL FOR GAS TURBINE ENGINE |
摘要 |
One exemplary embodiment of this disclosure relates to a gas turbine engine including a first engine component and a second engine component. The first engine component has a mate face adjacent a mate face of the second engine component. The engine further includes a seal between the mate face of the first engine component and the mate face of the second engine component. The seal establishes three points of contact with each mate face in at least one condition. |
申请公布号 |
EP3039269(A4) |
申请公布日期 |
2016.09.07 |
申请号 |
EP20140838947 |
申请日期 |
2014.08.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SNYDER, BROOKS E.;SLAVENS, THOMAS N.;BLAKE, MOSHESHE CAMARA-KHARY |
分类号 |
F02C7/28;F01D11/00;F04D29/08;F16J15/08 |
主分类号 |
F02C7/28 |
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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