| 发明名称 |
NOZZLE SUPPORT SYSTEM |
| 摘要 |
A nozzle support system for a nozzle of a gas turbine includes an outer ring, an inner ring disposed within the outer ring, and a plurality of links pivotally attaching the outer ring to the inner ring. Each one of the links may have an outer end that is pivotally attached to the outer ring, and each one of the links may have an inner end that is pivotally attached to the inner ring, such that the inner ring moves along a longitudinal axis of the outer ring. |
| 申请公布号 |
US2016115904(A1) |
申请公布日期 |
2016.04.28 |
| 申请号 |
US201514923669 |
申请日期 |
2015.10.27 |
| 申请人 |
Rolls-Royce North American Technologies, Inc. |
发明人 |
Sutterfield David L.;Yount Randall E. |
| 分类号 |
F02K1/78;F02C7/20;F16B1/00;F16M13/02;F16M11/06;F16M11/20;F02C3/04;F01D9/04 |
主分类号 |
F02K1/78 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A nozzle support system for a gas turbine, comprising:
an outer ring; an inner ring disposed within the outer ring; and a plurality of links pivotally attaching the outer ring to the inner ring; wherein each one of the links has an outer end that is pivotally attached to the outer ring, and each one of the links has an inner end that is pivotally attached to the inner ring, such that the inner ring moves along a longitudinal axis of the outer ring. |
| 地址 |
Indianapolis IN US |
