| 发明名称 |
GAS TURBINE ENGINE VANE EMBEDDED BEAM INTERRUPT OPTICAL TIP-TIMING PROBE SYSTEM |
| 摘要 |
A method of observing an airflow passage within a gas turbine engine includes locating a support in view of an airflow passage and housing an optical fiber within the support. |
| 申请公布号 |
US2014208837(A1) |
申请公布日期 |
2014.07.31 |
| 申请号 |
US201213725190 |
申请日期 |
2012.12.21 |
| 申请人 |
United Technologies Corporation |
发明人 |
Agoos Ian F.;Warren Eli C. |
| 分类号 |
G01M15/14 |
主分类号 |
G01M15/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of observing an airflow passage within a gas turbine engine, comprising:
locating a support in view of an airflow passage; and housing an optical fiber within the support. |
| 地址 |
US |
