Metal-base film thermocouple and preparation method thereof
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- UNIV OF ELECTRONIC SCI & TECH OF CHINA
- Publication Date
- 2010-11-24
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the field of sensor production technology and measurement technology for turbine blades, in particular to a thin-film thermocouple made of turbine engine blades to be measured as a substrate (material) and a production method thereof. This type of thermocouple can be widely used in Measure the surface temperature distribution of turbine engine blades, combustion chambers, etc., and provide corresponding basic data basis for the design of turbine engines. Background technique
[0002] In modern aero-engine technology, the harsh gas environment such as high temperature and high pressure generated by gas combustion will cause the surface temperature of the turbine blade and the combustion chamber to rise sharply, and at the same time generate a large thermal strain, while the temperature of the turbine blade and the surface of the combustion chamber The distribution and thermal strain have a great influence on the performance and ...