2016
DOI: 10.1179/1743284715y.0000000060
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Comparison of fatigue crack propagation in nickel base superalloys RR1000 and Udimet 720Li

Abstract: The effects of temperature, dwell and environment on the fatigue crack growth behaviour of two nickel base turbine disc superalloys RR1000 and Udimet 720Li are presented in the present paper. Fatigue tests were carried out at room temperature in air using a 20 Hz sinusoidal loading waveform and at elevated temperatures of 650 and 725°C in both air and vacuum environments using a trapezoidal loading waveform with dwell times at a maximum load of 1 or 20 s. The fatigue crack propagation resistance of both materi… Show more

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Cited by 16 publications
(14 citation statements)
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“…The values obtained for RR1000 show the same trend and are in line with the literature data, in particular with alloys Udimet 720LI and IN718 [15]. The agreement with alloy Udimet terms of composition [1,27]. However, with respect to the literature values, C12 and C44 correspond to the lower range, whereas C11 defines the upper limit.…”
Section: Figure 5 Experimentally Determined Reduced Young's Moduli Fsupporting
confidence: 89%
See 1 more Smart Citation
“…The values obtained for RR1000 show the same trend and are in line with the literature data, in particular with alloys Udimet 720LI and IN718 [15]. The agreement with alloy Udimet terms of composition [1,27]. However, with respect to the literature values, C12 and C44 correspond to the lower range, whereas C11 defines the upper limit.…”
Section: Figure 5 Experimentally Determined Reduced Young's Moduli Fsupporting
confidence: 89%
“…In terms of chemical composition, alloy RR1000 is relatively close Udimet 720LI. Accordingly, the stiffness properties of Udimet 720LI are the closest to those observed for RR1000 in this study (see Figure 6 and Figure 7), and the lower anisotropy ratio for RR1000 could be a result of its higher γ' volume fraction [27]. Furthermore, the effective modulus is not only dependent on the stiffness coefficients of the γ and γ' phase, but also on the γ' precipitate morphology and distribution.…”
Section: Figure 5 Experimentally Determined Reduced Young's Moduli Fsupporting
confidence: 72%
“…It is widely reported that the addition of a dwell period at maximum load at high temperature can significantly increase the crack growth rate per fatigue cycle in Ni-base superalloys [40][41][42][43][44][45][46][47][48][49][50][51][52]. Among these literature, Gustafsson et al [51,[53][54][55] has reported systematic results on the crack propagation behaviours with different dwell periods at different temperatures of a forged IN718.…”
Section: Accelerated Crack Propagationmentioning
confidence: 99%
“…was used. Table 1 lists the different heat treatment conditions used in this paper, based on previous heat treatments on RR1000 [7,8]. The as-received sample had followed the process route of solution heat treatment, aging (760°C/16 hrs) followed by forging.…”
Section: Methodsmentioning
confidence: 99%