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.
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.
| № | Author name | position | Name of organisation |
|---|---|---|---|
| 1 | Tuganov G.S. | teacher | Higher military aviation school |
| 2 | Mahmudov N.A. | teacher | Higher military aviation school |
| № | Name of reference |
|---|---|
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