| 发明名称 |
SYSTEM FOR SUPPORTING A TURBINE NOZZLE |
| 摘要 |
A system for supporting a turbine nozzle includes an inner barrel having a forward end, an aft end and an outer surface that extends between the forward end and the aft end. A first fitting that extends through the outer surface is defined within the inner barrel. The system further includes a nozzle support ring that defines a second fitting that is complementary to the first fitting defined within the inner barrel. |
| 申请公布号 |
US2014334925(A1) |
申请公布日期 |
2014.11.13 |
| 申请号 |
US201313891441 |
申请日期 |
2013.05.10 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Casavant Matthew Stephen;Black Kenneth Damon |
| 分类号 |
F01D25/24 |
主分类号 |
F01D25/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for supporting a turbine nozzle, comprising:
a. an inner barrel having a forward end, an aft end, an inner surface and an outer surface that extends between the forward end and the aft end; b. a first fitting defined within the inner barrel, wherein the first fitting extends through at least one of the inner surface or the outer surface; and c. a nozzle support ring defining a second fitting that is complementary to the first fitting. |
| 地址 |
Schenectady NY US |
