发明名称 |
ELECTRODYNAMIC MODAL TEST IMPACTOR SYSTEM AND METHOD |
摘要 |
<p>There is provided an electrodynamic modal test impactor system and method. The system has a controller device and an impactor assembly coupled to the controller device. The impactor assembly has a housing and a permanent magnet positioned within the housing. The impactor assembly further has a voice coil positioned within the housing in a magnetic gap of a magnetic yoke housing. The voice coil is driven by the controller device. The impactor assembly further has a drive shaft supported by two or more support elements. The drive shaft is attached to the voice coil and is driven by the voice coil. The impactor assembly further has a load cell attached to a free end of the drive shaft and a biasing device positioned within the magnetic yoke housing.</p> |
申请公布号 |
CA2829395(A1) |
申请公布日期 |
2014.05.30 |
申请号 |
CA20132829395 |
申请日期 |
2013.10.04 |
申请人 |
THE BOEING COMPANY |
发明人 |
POWERS, DONALD E.;KIISKILA, JASON C. |
分类号 |
G01M7/08 |
主分类号 |
G01M7/08 |
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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