TY - JOUR
T1 - 航空发动机涡轮叶片接触式测温技术应用进展
AU - Hu, Na
AU - Zhao, Wei
AU - Jin, Xiaochao
AU - Fan, Xueling
N1 - Publisher Copyright:
© 2023 Editorial Department of Advances in Aeronautical Science and Engineering. All rights reserved.
PY - 2023/2
Y1 - 2023/2
N2 - The temperature distribution of turbine blades can be revealed through the measurement, which is valuable for performance evaluation, failure analysis and optimization design of turbine blade. The higher requirement for the temperature measurement technique of aero-engine is put forward by continuously increasing of turbine inlet temperature. Three types of contact temperature measurement technologies for turbine blade are primarily introduced in this paper, including thin film thermocouple, crystal temperature sensor and temperature sensitive paint. The working principles are illustrated briefly. The application status at home and abroad is reviewed. The advantages and drawbacks are summarized, and the development direction of the three temperature measurement technologies is discussed.
AB - The temperature distribution of turbine blades can be revealed through the measurement, which is valuable for performance evaluation, failure analysis and optimization design of turbine blade. The higher requirement for the temperature measurement technique of aero-engine is put forward by continuously increasing of turbine inlet temperature. Three types of contact temperature measurement technologies for turbine blade are primarily introduced in this paper, including thin film thermocouple, crystal temperature sensor and temperature sensitive paint. The working principles are illustrated briefly. The application status at home and abroad is reviewed. The advantages and drawbacks are summarized, and the development direction of the three temperature measurement technologies is discussed.
KW - aero-engine
KW - contact temperature measurement
KW - crystal temperature sensor
KW - temperature sensitive paint
KW - thin film thermocouple
KW - turbine blade
UR - https://www.scopus.com/pages/publications/85193602958
U2 - 10.16615/j.cnki.1674-8190.2023.01.01
DO - 10.16615/j.cnki.1674-8190.2023.01.01
M3 - 文献综述
AN - SCOPUS:85193602958
SN - 1674-8190
VL - 14
SP - 1
EP - 12
JO - Advances in Aeronautical Science and Engineering
JF - Advances in Aeronautical Science and Engineering
IS - 1
ER -