Issue 35

T. Sadowski et alii, Frattura ed Integrità Strutturale, 35 (2016) 492-499; DOI: 10.3221/IGF-ESIS.35.55 497 two pieces (Fig. 12) took place respectively after 180 and 130 cycles, at which the quantity of the damaged FE was equal to at least 10%. 35800 rot/min 0 2 4 6 8 10 12 30 50 70 90 110 130 150 170 quantity of cycles quantity of damage elements [%] temp. 1300C temp. 1000C Figure 10: Quantity of the damaged elements versus the number of thermal cycles. The most important conclusion for industrial applications can be formulated as follows: the thermo-mechanical fstigue damage does not take place for the rotor speed up to 35 800 rot/min and for the level of temperature below 1000 0 C. The next step of numerical analysis the blade was heated cyclically to temperature 900 0 C and then its rotator speed was increased continuously. The fatigue failure took place only for the rotor speed equal to or higher than 42 970 rot/min. This value considerably exceeded the nominal speed level designed for the air-engines. The further speed increase up to 43 500 rot/min significantly reduces the number of safe cycles to the failure. Fig. 11 presents correlation between the relative quantity of damaged FE related to the number of thermal cycles. 0 2 4 6 8 10 40 60 80 100 120 140 160 180 200 220 quantity of cycles quantity of damage elements [%] 42970 rot/min 43500 rot/min Figure 11: Quantity of the damaged finite elements versus the number of thermal cycles (Temperature 900°C). The development of damage in dependence of number of thermal cycles for blade without TBC barrier Fig. 12 shows the bottom part of the blade for different quantities of cyclic thermo – mechanical loadings for the maximum amplitude of the temperature equal to 1300 0 C and the rotator speed 35 800 rot/min.