The crack growth rate of superalloy GH761 disk for turbine at 650℃ fatigue and creep interaction was tested. The test results show that with initial stress strength ΔK(K)=30 MN/m 3/2 and holding load for 90 seconds at 650 ℃, the crack growth rate of superalloy GH761 was fast, a nd the slope change of growth rate was not appreciable.
The results show that the alloy with both kinds of G. B. state are all not agreement with Linear - Damage Summation, t/tr +Nj/Nf = 1 under conditions of temperatuers 750, 800, 850, and 900℃, and hold time 0-32(min).
According to the Chinese (also ISO) standard for cement test, the loading rate of the electrohydraulic loading subsystem should be at 2.4 KN/s withan error less than 7% and error rate for the constant force control should be maintained within a range 0.2% .
The sawtooth nature of the curves is a consequence of load holding and relaxation during Raman scan.
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This paper dealt with the effect of dwell time at max. stress on the fatigue-creep interaction behavior of superalloy ECD.The results indicated that the cycle number of fracture decreased as the time of dwell at max. stress increased, However, the shape of interaction curve was not changed.The dwell at max stress intensified the creep effect resulting in the expansion of the interaction regions with predominant creep fracture ( i, e.CC, CFC regions ) , and the FC mixed region moved to the area with high alt...
The behaviour of cyclic endurance failure have been researched under different conditions of temperature and hold time. Two kinds of heat treatment method are used to get the different structure of grain boundary. The results show that the alloy with both kinds of G.B. state are all not agreement with Linear - Damage Summation, t/tr +Nj/Nf = 1 under conditions of temperatuers 750, 800, 850, and 900℃, and hold time 0-32(min). In general, all specimens are strengthened very clearly. There is great influence o...
The notch effect on high temperature LCF (Low Cycle Fatigue) and fatigue/creep interaction behaviour was investigated in GH33A super-alloy. LCF life was decreased dramatically because of notch and acuity of notchs. During LCF tests, dwelling at maximum stress introduces creep damage into low cycle fatigue, then decreased LCF fatigue cycles. At LCF tests with constant maximum stress and varied minimun stress, fatigue/creep interaction curve exhibits a maximum fatigue life at certain stress condition and frac...