发明名称 Automated analysis of turbine component thermal response
摘要 In accordance with a first aspect of the present invention, thermal response of a turbine component to application of thermal stimuli is automatically analyzed by regions of interest. In accordance with another aspect, each region is analyzed for conformance for a number of thermal response metrics, in an absolute sense, and/or relative to each other. In one embodiment, the thermal response metrics include the temperature threshold a particular region (e.g. the reference/primary region) exhibits a critical response size, and that the sub-region achieving the critical response size at the temperature threshold also has a critical shape. In one embodiment, the analyses are performed using the pixel values of the constituting pixels of a picture frame of the turbine component's thermal response. In accordance with yet another aspect, a binary passed or failed conclusion is reached based on the results of the automated analyses.
申请公布号 US2003100987(A1) 申请公布日期 2003.05.29
申请号 US20010006436 申请日期 2001.11.21
申请人 BROWN WILLIAM T.;DALIO BRIAN A. 发明人 BROWN WILLIAM T.;DALIO BRIAN A.
分类号 G01K7/42;(IPC1-7):G06F19/00 主分类号 G01K7/42
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