Abstract Influence of the free air temperature during aircraft takeoff and engine operating time upon the cyclic life of an aircraft GTE turbine disk made from the heat-resistance deformable nickel-base alloy is analyzed and the variation of engine operating parameters in the process of service is taken into account.
Variation of aircraft GTE turbine disks cyclic life depending on operational factors
Russian Aeronautics (Iz VUZ) ; 54 , 2 ; 213-216
01.06.2011
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch