Temperature Measurement in Aircraft Engine Manufacturing: Thermocouple Calibration Systems

In the research, development, manufacturing and production of aircraft engines and gas turbine units, thermocouples are widely used to measure and control temperatures in high-temperature environments. For example, it can measure key parameters such as the temperature in the combustion chamber of an aircraft engine and the exhaust temperature of a steam turbine, which is essential to ensure the safety and reliability of aircraft engines. In order to ensure the accuracy and reliability of thermocouples, a thermocouple calibration system is needed.

During long-term use, the performance of thermocouples may be affected by various factors, resulting in measurement errors. The thermocouple calibration system can simulate various temperature environments, calibrate and test thermocouples, and promptly detect and correct errors, thereby ensuring that thermocouples can provide accurate temperature data in actual use.

The ZRJ-23 thermocouple calibration system is a highly integrated automated calibration system, mainly composed of computers, printers, high-precision digital multimeters, multi-channel scanning controllers, thermocouple calibration furnaces, constant temperature baths and other components. It can automatically complete the mass calibration of various temperature instruments such as thermocouples, and has the characteristics of high precision, high efficiency and high automation.

Thermocouples play a vital role in the research, development, manufacturing and production of aircraft engines and gas turbine units, and the thermocouple calibration system is an important tool to ensure the accuracy and reliability of thermocouples. Through the thermocouple calibration system detection, users can promptly discover and correct the errors of thermocouples to ensure that their performance meets the design requirements.