Integrated Fabrication of High-Temperature Microelectromechanical System Sensor on Aeroengine Turbine Blade-Reference-Cited by-同舟云学术

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Integrated Fabrication of High-Temperature Microelectromechanical System Sensor on Aeroengine Turbine Blade

Published:2018-07 Issue:3 Volume:32 Page:828-830
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Duan Franklin Li¹,Li Jibao²,Gao Junchao³,Ding Guifu¹,Cao Xueqiang⁴

Affiliation:

1. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China

2. AVIC Commercial Aircraft Engine Company, Ltd., 201108 Shanghai, People’s Republic of China

3. Huawei Technologies Company, Ltd., 200240 Shanghai, People’s Republic of China

4. Wuhan University of Technology, 430070 Hubei, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.T5147

Reference14 articles.

1. An Overview of High-Temperature Electronics and Sensor Development at NASA Glenn Research Center

2. Durable Heat Flux Sensor for Extreme Temperature and Heat Flux Environments

3. An Efficient Method for Calculating Surface Temperature and Heat Flux Based on Embedded Temperature Sensors

4. Improving the accuracy of temperature measurements

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5. Accurate Real-Time Temperature Measurement Method in Ultra-High Temperature Rotational Environments for Aero Engines/Turbines;IEEE Sensors Journal;2022-04-01

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