FIELD: engines and pumps.
SUBSTANCE: method is applied for monitoring of a vibration state of aircraft GTE both on ground processing devices and in real time in onboard engine control systems.
EFFECT: obtaining high reliability parameters of GTE vibration diagnostic results immediately under operating conditions by means of all-around consideration of factors determining vibration state of GTEs at their operation on the ground and under flight conditions.
6 cl, 1 dwg
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