A Method of Improving the Measuring Accuracy of Stagnation Total Temperature Probe

Abstract

The invention relates to a method for improving the measurement accuracy of a stagnation type total temperature probe. A deflector is arranged at the stagnation cover inlet and a stagnation chamber, and the stagnation cover inlet is divided into upper and lower parts. The present invention can better organize the stagnation of indoor airflow, make the distribution of airflow velocity around the measurement end of the stagnation type total temperature probe more uniform, reduce the pulsation of airflow, and can significantly reduce the airflow velocity impacting the measurement end, reducing stagnation The speed error of the stagnant total temperature probe can be reduced, thereby improving the measurement accuracy of the stagnant total temperature probe.

Description

technical field [0001] The invention relates to a method for improving the measurement accuracy of a stagnation total temperature probe, in particular to the measurement of total temperature of aero-engines or gas turbines and high-speed airflow in the field of aerospace. Background technique [0002] The temperature indicated by the total temperature probe when measuring the airflow temperature is essentially the temperature of the part of the airflow that impacts its measuring end and exchanges heat with it. total air temperature T t From static temperature T s and dynamic temperature T d T t =T s +T d , where the magnitude of the dynamic temperature is positively correlated with the quadratic of the air velocity, as shown in formula (1). It can be seen that if the airflow flowing through the temperature measuring end of the total temperature probe has a relatively high velocity, the temperature value indicated by the total temperature probe will be quite different f...

AI Technical Summary

Problems solved by technology

[0010] Although the stagnant total temperature probe has many advantages in the measurement of the total temperature of the high-speed airflow, due to the lack of understanding and analysis of the characteristics of the flow structure in the stagnant chamber, there are still many shortcomings in the current technology.

First, in the currently used technology, the airflow vertically impacts the inner wall of the stagnation chamber and forms multiple separation zones in the stagnation chamber. stagnation effect

Second, due to the influence of the separation bubble in the stagnation chamber, the flow of the airflow in the stagnation chamber has a strong three-dimensional unsteadiness, which makes the airflow velocity V around the measuring end vary in size and the distribution is very uneven

Third, this strong three-dimensional unsteadiness makes the pulsation of the airflow flowing through the measurement end larger, which increases the pulsation of the measured airflow temperature and reduces the temperature measurement accuracy

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