Device and method for testing a gas turbine engine component
US8720259B1 · kind B1 · utility
2Cited by
8References
17Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 10, 2012 |
| Grant date | May 13, 2014 |
| Priority date | — |
| Expiry date | Dec 18, 2032 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG01M15/14
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.