发明名称 |
Seal for a turbine engine, turbine engine arrangement, and corresponding method of production |
摘要 |
In one aspect, a seal for a turbine engine (10) includes a seal body (38) disposed at a base of a turbine engine blade (22) and a wing portion (46) extending axially from said seal body. The wing portion has a first portion (52, 54) substantially parallel with a centerline (C) of the engine and an angled upturn portion (48). The first portion extends between the seal body and the angled upturn portion (48). An angle (A) between the engine centerline and the angled upturn portion (48) is between about 0 degrees and about 90 degrees. Corresponding turbine engine arrangement and method of production are also provided. |
申请公布号 |
EP2634375(A3) |
申请公布日期 |
2016.10.26 |
申请号 |
EP20130157045 |
申请日期 |
2013.02.27 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
PIERSALL, MATTHEW ROBERT;KAREFF, SPENCER AARON |
分类号 |
F01D11/00;F01D5/30;F01D11/02 |
主分类号 |
F01D11/00 |
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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