The results of the probabilistic assessment of life for the low-pressure compressor rotor of the gas turbine engine for a regional aircraft are presented taking into account production tolerances. The calculation algorithm, preparation of the probabilistic model parameters, and the experimental program of automated probabilistic analysis are described, the example of the life calculation results is given.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Russ. Aeronaut.
Russian Aeronautics ; 62 , 3 ; 455-462
2019-07-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
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