| 发明名称 |
TURBINE BLADE PLATFORM SEAL ASSEMBLY VALIDATION |
| 摘要 |
A platform seal assembly for a gas turbine engine with a turbine disk and a plurality of turbine blades is disclosed. The platform seal assembly includes a platform seal and a validation tab. The platform seal includes a first end, a second end, opposite and distal to the first end, and a body extending between the first end and the second end. The validation tab includes an attachment portion affixed to the platform seal and an observable indicator portion extending from the attachment portion. |
| 申请公布号 |
US2015204245(A1) |
申请公布日期 |
2015.07.23 |
| 申请号 |
US201414159830 |
申请日期 |
2014.01.21 |
| 申请人 |
SOLAR TURBINES INCORPORATED |
发明人 |
Marasco Angelo Vincent;Lamicq Olivier Jacques Louis |
| 分类号 |
F02C7/28 |
主分类号 |
F02C7/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A platform seal assembly for a gas turbine engine with a turbine disk and a plurality of turbine blades, the platform seal assembly comprising:
a platform seal including
a first end,a second end, opposite and distal to the first end, and a body extending between the first end and the second end; and a validation tab including
an attachment portion affixed to the platform seal, andan observable indicator portion extending from the attachment portion. |
| 地址 |
San Diego CA US |
