@inproceedings{d243ed9d3dee42a48b776be73489687f,
title = "Simulation of High Temperature Thin Film Thermocouple on Engine Blade Surface",
abstract = "In order to avoid the instability flutter of aero-engine blade and prevent the failure of thin film thermocouple caused by the blade in complex environment, the structural strength of the thermocouple on the actual blade surface was studied in this paper. Firstly, based on the 3D scanning of the real blade, the blade model is established after the point cloud graphics. The surface thermocouple model of the blade is established in Solidworks for simulation, and the modal and harmonic response analysis of the blade is simulated. Secondly, the vibration of the curved thin film thermocouple and the stress distribution of the blade under the acceleration shock were studied in Comsol, and the failure weakness was analyzed to avoid the failure of the thin film thermocouple caused by the bending, fracture or shedding of the thin film thermocouple on the blade due to vibration and shock, providing the most suitable thermocouple selection for the engine blade.",
keywords = "Engine blade, high temperature, simulation, thin film thermocouple",
author = "Meiju Zhang and Bian Tian and Rong Ma and Manguo Huang and Xiaobo Liang and Jiangjiang Liu and Zhongkai Zhang",
note = "Publisher Copyright: {\textcopyright} 2022 The authors and IOS Press.; 2022 International Conference on Mechatronics and Automation Technology, ICMAT 2022 ; Conference date: 29-10-2022 Through 30-10-2022",
year = "2022",
month = dec,
day = "15",
doi = "10.3233/ATDE221166",
language = "英语",
series = "Advances in Transdisciplinary Engineering",
publisher = "IOS Press BV",
pages = "196--201",
editor = "Jinyang Xu",
booktitle = "Moving Integrated Product Development to Service Clouds in the Global Economy - Proceedings of the 21st ISPE Inc. International Conference on Concurrent Engineering, CE 2014",
}