发明名称 Infrared NDI device for shallow defect detection
摘要 First and second thermal sensors measure the respective temperatures of portions of a surface of a structure such as an aircraft component. An alert signal emitted if the temperatures of the surface portions are substantially different. An energy source causes heat flow within the structure. Subsurface flaws such as disbonded areas between composite layers and foreign materials obstruct heat flow within the structure and cause proximate surface portions to exhibit different temperatures. A non-alert signal may be emitted if the temperatures of proximate surface portions are essentially the same.
申请公布号 GB2455694(A) 申请公布日期 2009.06.24
申请号 GB20090007510 申请日期 2007.10.10
申请人 THE BOEING COMPANY 发明人 JEFFREY G THOMPSON;JEFFREY R KOLLGAARD;CLYDE T UYEHARA
分类号 G01N25/72;B64F5/00;G01N21/88 主分类号 G01N25/72
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