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Gas turbine component coating thickness, hardness or porosity parameter measurement procedure measures time dependence of heat emitted after heating by flash lamp
Gas turbine component coating thickness, hardness or porosity parameter measurement procedure measures time dependence of heat emitted after heating by flash lamp
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机译:燃气轮机组件涂层厚度,硬度或孔隙率参数测量程序可测量闪光灯加热后散发的热量的时间依赖性
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摘要
A gas turbine component coating thickness, hardness or porosity parameter measurement procedure warms the surface (170) using a laser or flash lamp (120) for preset power and time and measures the emitted radiation (210) using a pyrometer (110), thermal camera or infrared line sensor and calculates (100) the parameter as a function of the time dependence. Independent claims are included for equipment using the procedure.
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