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RESEARCHING OF EMPIRICAL DISTRIBUTIONS OF RANDOM VALUES OF ROTOR VIBRATION OF A GAS TURBINE ENGINE OF A HELICOPTER IN THE CONDITIONS OF MOUNTAIN DESERT OF THE REPUBLIC OF UZBEKISTAN

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The article presents the dynamic changes of the random vibration values of the front support of the gas turbine engine of the Mi-8MTV transport helicopter in the mountainous desert area of Uzbekistan. The subordination of empirical random vibration values to the normal Gaussian distribution is investigated. A comprehensive method for determining the technical condition of a helicopter GTE rotor during operation is presented, based on the measurement of vibration parameters and GTE oil temperature.

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# vibration# parameters of a gas turbine engi# distribution laws

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