Identification method for assessing the state vibration strength of the aircraft engine

2020

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DOI 10.47533/2020.1606-146x.27
Data confidence 70 medium
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Abstract

A method foraircraft engine state assessment is described, based on the theory of identification measurements and consisting in the analysis of the regularity properties of the temporal and correlation functions of the vibration signal. An example of an aircraft engine dynamics analysis during flight tests is considered. Four classes of states are distinguished according to the “norm – defect” scale.