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Non destructive monitoring of microstructure changes of a component ( layer system, turbine blades, liners of a combustion chamber )

机译:组件(层系统,涡轮叶片,燃烧室衬里)微观结构变化的无损监测

摘要

Method for monitoring degradation of a layer system caused by thermal and mechanical overloading. According to the method electrical, mechanical and or material parameters of the layer system are monitored over time by repeated measurement and comparison. An example of the method is monitoring a ceramic thermal insulation layer (10) in which pores (13) provide an effective thermal shock behavior. During use in a turbine the pores are sintered with a resultant reduction in the pore size (16). Thus to monitor degradation, pore size is measured over time.
机译:监视由热和机械过载引起的层系统退化的方法。根据该方法,通过重复的测量和比较,随时间监视层系统的电,机械和/或材料参数。该方法的一个示例是监测其中孔(13)提供有效热冲击行为的陶瓷绝热层(10)。在涡轮机中使用期间,孔被烧结,从而减小了孔径(16)。因此,为了监测降解,可随时间测量孔径。

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