发明名称 Method and apparatus for thermographically and quantitatively analyzing a structure for disbonds and/or inclusions
摘要 A heat source such as a magnetic induction/eddy current generator remotely heats a region of a surface of a test structure to a desired depth. For example, the frequency of the heating source can be varied to heat to the desired depth. A thermal sensor senses temperature changes in the heated region as a function of time. A computer compares these sensed temperature changes with calibration standards of a similar sample having known disbond and/or inclusion geography(ies) to analyze the test structure. A plurality of sensors can be arranged linearly to sense vector heat flow.
申请公布号 US5562345(A) 申请公布日期 1996.10.08
申请号 US19950571688 申请日期 1995.12.13
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 HEYMAN, JOSEPH S.;WINFREE, WILLIAM P.;CRAMER, K. ELLIOTT;ZALAMEDIA, JOSEPH N.
分类号 G01N25/72;(IPC1-7):G01N25/72 主分类号 G01N25/72
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