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Advanced Characterization Techniques for Turbine Blade Wear and Damage

机译:涡轮叶片磨损和损坏的高级表征技术

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摘要

This paper presents four complementary non-destructive measurement techniques for material characterization and damage detection of turbine blades. The techniques are macroscopic fringe projection with inverse fringe projection algorithms, robot guided microscale fringe projection, high frequency eddy current and pulsed high frequency induction thermography, both in the megahertz range. The specimen on which the measurements were carried out is a blade of the 1 st stage high pressure turbine of a modern airplane jet engine. The turbine blade was characterized with regard to the macroscopic and microscopic geometry, cracks in the base material as well as the condition of the protective layer system.
机译:本文介绍了四种互补的非破坏性测量技术,用于涡轮叶片的材料表征和损伤检测。这些技术是具有逆条纹投影算法的宏观条纹投影,机器人引导的微尺度条纹投影,高频涡流和脉冲高频感应热成像,均在兆赫兹范围内。在其上进行测量的样品是现代飞机喷气发动机的第一级高压涡轮的叶片。根据宏观和微观几何形状,基础材料中的裂纹以及保护层系统的状况来表征涡轮叶片。

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