Advances in application of contact temperature measurement technology for aero-engine blade
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 continuous...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2023-02-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022051 |
| _version_ | 1827943895862870016 |
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| author | HU Na ZHAO Wei JIN Xiaochao FAN Xueling |
| author_facet | HU Na ZHAO Wei JIN Xiaochao FAN Xueling |
| author_sort | HU Na |
| collection | DOAJ |
| description | 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. |
| first_indexed | 2024-03-13T10:22:14Z |
| format | Article |
| id | doaj.art-d8f50367b7044227bc3766baac980faa |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-03-13T10:22:14Z |
| publishDate | 2023-02-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-d8f50367b7044227bc3766baac980faa2023-05-20T08:56:58ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902023-02-0114111210.16615/j.cnki.1674-8190.2023.01.0120230101Advances in application of contact temperature measurement technology for aero-engine bladeHU Na0ZHAO Wei1JIN Xiaochao2FAN Xueling3School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an 710049, ChinaLaboratory of Strength Transmission Test Technology, AECC Sichuan Gas Turbine Establishment, Mianyang 621000, ChinaSchool of Aerospace Engineering, Xi'an Jiaotong University, Xi'an 710049, ChinaSchool of Aerospace Engineering, Xi'an Jiaotong University, Xi'an 710049, ChinaThe 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.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022051aero-engineturbine bladecontact temperature measurementthin film thermocouplecrystal temperature sensortemperature sensitive paint |
| spellingShingle | HU Na ZHAO Wei JIN Xiaochao FAN Xueling Advances in application of contact temperature measurement technology for aero-engine blade Hangkong gongcheng jinzhan aero-engine turbine blade contact temperature measurement thin film thermocouple crystal temperature sensor temperature sensitive paint |
| title | Advances in application of contact temperature measurement technology for aero-engine blade |
| title_full | Advances in application of contact temperature measurement technology for aero-engine blade |
| title_fullStr | Advances in application of contact temperature measurement technology for aero-engine blade |
| title_full_unstemmed | Advances in application of contact temperature measurement technology for aero-engine blade |
| title_short | Advances in application of contact temperature measurement technology for aero-engine blade |
| title_sort | advances in application of contact temperature measurement technology for aero engine blade |
| topic | aero-engine turbine blade contact temperature measurement thin film thermocouple crystal temperature sensor temperature sensitive paint |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022051 |
| work_keys_str_mv | AT huna advancesinapplicationofcontacttemperaturemeasurementtechnologyforaeroengineblade AT zhaowei advancesinapplicationofcontacttemperaturemeasurementtechnologyforaeroengineblade AT jinxiaochao advancesinapplicationofcontacttemperaturemeasurementtechnologyforaeroengineblade AT fanxueling advancesinapplicationofcontacttemperaturemeasurementtechnologyforaeroengineblade |