DIAGNOSTIC ANALYSIS OF RANDOM VIBRATION RESULTS IN THE AVIATION GAS TURBINE ENGINESPULSE-WIDTH AUTOMATIC CONTROL SYSTEMS BASED ON DYNAMIC GRAPHS

Authors

G. Sh. Tuganov, Academy of Armed Forces of Uzbekistan
C. M. Rakhimov, Academy of Armed Forces of Uzbekistan
E. Norkulov, Aircraft and engine of aviation military school

Abstract

Studies are often conducted to minimize the effect of vibration on equipment and its mechanisms. Since the engine is the main driving force of all technical objects, vibration is one of the factors hindering its operation. With this in mind, this article investigated the random probability distribution of vibration parameters using the laws of mathematical statistical distribution and was found to be compatible with the normal distribution law. At the same time, this study demonstrates that the proposed method of technical diagnostics can be used to assess helicopter engine failures.

First Page

13

Last Page

19

DOI

https://doi.org/10.51346/tstu-01.19.2.-77-0019

References

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Recommended Citation

Tuganov, G. Sh.; Rakhimov, C. M.; and Norkulov, E. (2019) "DIAGNOSTIC ANALYSIS OF RANDOM VIBRATION RESULTS IN THE AVIATION GAS TURBINE ENGINESPULSE-WIDTH AUTOMATIC CONTROL SYSTEMS BASED ON DYNAMIC GRAPHS," Technical science and innovation: Vol. 2019: Iss. 2, Article 1.
DOI: https://doi.org/10.51346/tstu-01.19.2.-77-0019
Available at: https://btstu.researchcommons.org/journal/vol2019/iss2/1