发明名称 |
Blade outer air seal with improved thermomechanical fatigue life |
摘要 |
A blade outer air seal (20) for a gas turbine has an abradable coating (22) with a substantially uniform thickness during service use. Prior to being placed in service, the abradable coating has a central portion (34C) with a greater thickness (t 2 ) than leading and trailing portions (34L; 34T). When placed in service, the blade outer air seal is positioned so that the central portion of the abradable coating with the greater thickness is located in a blade rub path of the turbine blades. As a result of abrasion in the blade rub path, the thickness of the central portion of the abradable coating is reduced so that it becomes substantially similar to the thickness (t 1 ) of the leading and trailing portions. |
申请公布号 |
EP2053202(A2) |
申请公布日期 |
2009.04.29 |
申请号 |
EP20080253487 |
申请日期 |
2008.10.27 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
STROCK, CHRISTOPHER W.;BELANGER, PHILIP R. |
分类号 |
F01D11/12 |
主分类号 |
F01D11/12 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|