| 发明名称 |
HEATSHIELD DISCOURAGER SEAL FOR A GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine includes a service line interface that extends from an outer surface of a bearing support such that a heat shield is spaced from the outer surface. A method of mounting a heat shield to a gas turbine engine includes trapping a heat shield within a gapped overlap spaced from an outer surface of a bearing support. |
| 申请公布号 |
US2016032763(A1) |
申请公布日期 |
2016.02.04 |
| 申请号 |
US201414774931 |
申请日期 |
2014.03.14 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Grogg Gary L;Szymanski Grace E |
| 分类号 |
F01D25/08;F01D25/18;F01D25/16 |
主分类号 |
F01D25/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a service line interface to define a gapped overlap that at least partially supports a heat shield. |
| 地址 |
Hartford CT US |
