1979
DOI: 10.1007/bf00550720
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The fracture and fatigue of sintered diamond compact

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Cited by 27 publications
(6 citation statements)
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“…Wear was only detected after an incubation period, which decreased as the hardness of the second material increased, but which was always finite. Results showing that sintered diamond compacts can show fatigue in drilling experiments have been given by Dunn and Lee [116].…”
Section: Fatiguementioning
confidence: 85%
“…Wear was only detected after an incubation period, which decreased as the hardness of the second material increased, but which was always finite. Results showing that sintered diamond compacts can show fatigue in drilling experiments have been given by Dunn and Lee [116].…”
Section: Fatiguementioning
confidence: 85%
“…Gross fracturing of relatively un--worn cutters was found as the predominant failure mechanism. Dunn and Lee [14] performed fatigue tests on sintered PDC and, like Moseley et al [4] and Zacny [6], also reported a reduction in fracture stress due to repeated loading. In addition, Dunn and Lee suggested that fatigue in PDC was likely to be caused by some irreversible processes involving opening and closing of sub--critical cracks followed by the gradual growth of the same [14].…”
Section: Introductionmentioning
confidence: 92%
“…The researchers seem to be very divided about this point. For instance, Dunn and Lee [22] suggested that mechanical overloading of the cutters and a subsequent brittle crack propagation are the main causes of failure. On the opposite, Sneddon and Hall [23] considered fatigue crack growth as a possible dominant fracture mechanism, since cutters are repeatedly subjected to impacts.…”
Section: Experimental Observation Of Failure Modes and Proposed Classmentioning
confidence: 99%
“…5. Considering P * = 2000 N as the typical peak value of the impact force experienced during experimental tests [22], the nondimensional critical load corresponding to crack propagation, P c /P * , is depicted in Fig. 6 as a function of the relative crack depth, a/a max , where a max denotes the crack length at failure, i.e.…”
Section: Chipping Failure Modesmentioning
confidence: 99%