Siddiqui Sanna F, Knipe Kevin, Manero Albert, Meid Carla, Wischek Janine, Okasinski John, Almer Jonathan, Karlsson Anette M, Bartsch Marion, Raghavan Seetha
Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, Florida 32816, USA.
Rev Sci Instrum. 2013 Aug;84(8):083904. doi: 10.1063/1.4817543.
Measurement techniques to obtain accurate in situ synchrotron strain measurements of thermal barrier coating systems (TBCs) applied to hollow cylindrical specimens are presented in this work. The Electron Beam Physical Vapor Deposition coated specimens with internal cooling were designed to achieve realistic temperature gradients over the TBC coated material such as that occurring in the turbine blades of aeroengines. Effects of the circular cross section on the x-ray diffraction (XRD) measurements in the various layers, including the thermally grown oxide, are investigated using high-energy synchrotron x-rays. Multiple approaches for beam penetration including collection, tangential, and normal to the layers, along with variations in collection parameters are compared for their ability to attain high-resolution XRD data from the internal layers. This study displays the ability to monitor in situ, the response of the internal layers within the TBC, while implementing a thermal gradient across the thickness of the coated sample. The thermal setup maintained coating surface temperatures in the range of operating conditions, while monitoring the substrate cooling, for a controlled thermal gradient. Through variation in measurement location and beam parameters, sufficient intensities are obtained from the internal layers which can be used for depth resolved strain measurements. Results are used to establish the various techniques for obtaining XRD measurements through multi-layered coating systems and their outcomes will pave the way towards goals in achieving realistic in situ testing of these coatings.
本文介绍了用于获取涂覆在空心圆柱试样上的热障涂层系统(TBC)原位同步加速器精确应变测量的技术。设计了具有内部冷却功能的电子束物理气相沉积涂层试样,以在TBC涂层材料上实现实际的温度梯度,如航空发动机涡轮叶片中出现的温度梯度。使用高能同步加速器X射线研究了圆形横截面在包括热生长氧化物在内的各层中对X射线衍射(XRD)测量的影响。比较了包括沿层收集、切向和法线方向的多种光束穿透方法以及收集参数的变化,以评估它们从内层获取高分辨率XRD数据的能力。本研究展示了在涂覆样品厚度方向施加热梯度的同时,原位监测TBC内层响应的能力。热装置在监测基材冷却的同时,将涂层表面温度维持在工作条件范围内,以实现可控的热梯度。通过改变测量位置和光束参数,从内层获得了足够的强度,可用于深度分辨应变测量。研究结果用于确定通过多层涂层系统进行XRD测量的各种技术,其成果将为实现这些涂层实际原位测试的目标铺平道路。