| 发明名称 |
ASSEMBLIES AND METHODS FOR MONITORING TURBINE COMPONENT STRAIN |
| 摘要 |
Assemblies and methods for monitoring turbine component deformation are provided. An assembly includes a first strain sensor configurable on the turbine component, the first strain sensor including at least two reference points and having a first dimension. The assembly further includes a second strain sensor configurable on the turbine component, the second strain sensor including at least two reference points and having a first dimension which corresponds to the first dimension of the first strain sensor. An initial value of the first dimension of the second strain sensor is different from an initial value of the first dimension of the first strain sensor. In accordance with another embodiment of the present disclosure, a method for monitoring turbine component deformation is provided. |
| 申请公布号 |
US2016319694(A1) |
申请公布日期 |
2016.11.03 |
| 申请号 |
US201514697766 |
申请日期 |
2015.04.28 |
| 申请人 |
General Electric Company |
发明人 |
Hovis Gregory Lee;Nickles Blake Ashton;Ranson William F.;Davidoff Robert William |
| 分类号 |
F01D21/00;G01L1/22 |
主分类号 |
F01D21/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for monitoring turbine component deformation, the assembly comprising:
a first strain sensor configurable on the turbine component, the first strain sensor comprising at least two reference points and having a first dimension; a second strain sensor configurable on the turbine component, the second strain sensor comprising at least two reference points and having a first dimension which corresponds to the first dimension of the first strain sensor, wherein an initial value of the first dimension of the second strain sensor is different from an initial value of the first dimension of the first strain sensor. |
| 地址 |
Schenectady NY US |
