发明名称 |
Device for detecting a crack on a turbine blade of an aircraft engine |
摘要 |
An apparatus for inspecting a turbine blade of an aircraft engine may include a shaft having a proximate end and a distal end, an attachment device coupled to the distal end of the shaft and capable of being attached to a strut of the aircraft engine and an engagement device, coupled to the attachment device, capable of moving away from the attachment device and attaching to a trailing edge of the turbine blade. The apparatus may also include a probe moveably coupled to the engagement device and capable of moving along a leading edge of the turbine blade to detect a surface anomaly of the turbine blade and a control device for controlling the movement of the probe along the leading edge of the turbine engine in response to user manipulation.
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申请公布号 |
US2005068050(A1) |
申请公布日期 |
2005.03.31 |
申请号 |
US20030672444 |
申请日期 |
2003.09.26 |
申请人 |
DUFFY TIMOTHY R.;PEREZ-RUBERTE EDDIE;SEDA MARISOL |
发明人 |
DUFFY TIMOTHY R.;PEREZ-RUBERTE EDDIE;SEDA MARISOL |
分类号 |
G01M5/00;G01R27/08;(IPC1-7):G01R27/08 |
主分类号 |
G01M5/00 |
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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