发明名称 ULTRASONIC PROBE FOR HOLLOW FUSE PIN INSPECTION
摘要 A self-aligning probe assembly has one or more ultrasonic transducers adapted to transmit an ultrasonic shear wave into the inside surface of the hollow structure such as an aircraft fuse pin and to receive the shear wave emerging from the inside surface of the hollow structure. The nature of the received shear wave indicates the presence of flaws or damage in the inspected part. The probe assembly can be used to inspect fuse pins on aircraft without having to remove the aircraft engines.
申请公布号 US2008148856(A1) 申请公布日期 2008.06.26
申请号 US20060615505 申请日期 2006.12.22
申请人 THE BOEING COMPANY 发明人 GEORGESON GARY E.;LEE JAMES H.;SAFAI MORTEZA;FREET MARTIN L.
分类号 G01N29/04 主分类号 G01N29/04
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