发明名称 |
Airflow testing method and system for multiple cavity blades and vanes |
摘要 |
A system for airflow testing a turbine engine component having multiple cavities has a test fixture with a module for supporting a turbine engine component to be tested and a sliding element for sequentially allowing a pressurized fluid to flow through each of the multiple cavities in the turbine engine component. A method for performing the airflow testing is also described.
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申请公布号 |
US8534122(B2) |
申请公布日期 |
2013.09.17 |
申请号 |
US201113337525 |
申请日期 |
2011.12.27 |
申请人 |
MIRONETS SERGEY;DAVIS THOMAS R.;VARSELL RICHARD;PIETRASZKIEWICZ EDWARD;UNITED TECHNOLOGIES CORPORATION |
发明人 |
MIRONETS SERGEY;DAVIS THOMAS R.;VARSELL RICHARD;PIETRASZKIEWICZ EDWARD |
分类号 |
G01M15/14 |
主分类号 |
G01M15/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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