发明名称 |
Device and method for testing a gas turbine engine component |
摘要 |
An exemplary device for testing a gas turbine engine component includes a shaft that is configured to be rotated. A first hub is selectively fixed to the shaft near a first end of the first hub with an opposite, second end spaced from the shaft. A second hub is selectively fixed to the shaft near a first end of the second hub with an opposite, second end spaced from the shaft. The second ends of the hubs each have a feature for supporting the component between the first and second hubs at a location spaced from the shaft for introducing a load on the component near the location. |
申请公布号 |
US8720259(B1) |
申请公布日期 |
2014.05.13 |
申请号 |
US201213709498 |
申请日期 |
2012.12.10 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BENJAMIN DANIEL;BALAMURUGAN KALIYA;BERKLEY ROBERT B.;WILLISTON ROBERT L. |
分类号 |
G01M1/04 |
主分类号 |
G01M1/04 |
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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