发明名称 |
SEALS FOR A CIRCUMFERENTIAL STOP RING IN A TURBINE EXHAUST CASE |
摘要 |
A turbine seal system comprises an annular structural frame, a circumferential ring, a fairing and a seal. The circumferential ring is joined to the annular structural frame. The fairing is disposed within the annular structural frame and is engaged with the circumferential ring to limit circumferential rotation of the fairing with respect to the annular structural frame. The seal extends between the fairing and the circumferential ring. In one embodiment, the structural component comprises a ring-strut-ring turbine exhaust case. |
申请公布号 |
WO2014143317(A3) |
申请公布日期 |
2014.12.24 |
申请号 |
WO2013US76758 |
申请日期 |
2013.12.19 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BUDNICK, MATTHEW;CHUONG, CONWAY;SCOTT, JONATHAN A. |
分类号 |
F01D11/00;F01D9/04;F02C7/28 |
主分类号 |
F01D11/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|