An investigation of the roles of crack initiation, propagation and ratchetting in producing wear in metallic sliding contacts

Author(s):  
J Liu ◽  
E. M. Kopalinsky ◽  
P. L. B. Oxley

Experiments are described in which the edge of a hard wedge is loaded against the periphery of a rotating disc of softer specimen material. The normal and frictional forces and inward movement of the wedge as the disc wears are continually monitored throughout a test. The results obtained are used together with measurements of the wearing surfaces of metallographic sections to test a newly proposed wear model. In this model it is assumed that ratchetting causes failure of the surface and hence the production of wear particles, while low-cycle fatigue determines the crack propagation rate and hence the wear rate.

2007 ◽  
Vol 353-358 ◽  
pp. 2962-2965
Author(s):  
Masao Sakane ◽  
Kazuhiro Itoh ◽  
Yutaka Tsukada ◽  
Kenji Terada

This paper studies the crack propagation at Sn37Pb-copper interface in push-pull low cycle fatigue. Bonded specimens of Sn37Pb and copper having notch holes with different distances from the interface were fatigued at 313K and the crack propagation paths were observed. Cracks propagated at the interface when the notch hole was near the interface but propagated in the solder when the notch hole was away from the interface. The propagation rate of the interfacial crack was faster than that of non-interface crack. The crack path and crack propagation rate of the two types of cracks were discussed in relation to J integral range calculated by finite element method.


1971 ◽  
Vol 14 (69) ◽  
pp. 191-198
Author(s):  
Eiryo SHIRATORI ◽  
Shin-ichiro NISHI ◽  
Akio IIDA ◽  
Takeshi Ichikawa

2019 ◽  
Vol 9 (18) ◽  
pp. 3825 ◽  
Author(s):  
Giacomo Canale ◽  
Moustafa Kinawy ◽  
Angelo Maligno ◽  
Prabhakar Sathujoda ◽  
Roberto Citarella

Aerospace structures must be designed in such a way so as to be able to withstand even more flight cycles and/or increased loads. Damage tolerance analysis could be exploited more and more to study, understand, and calculate the residual life of a component when a crack occurs in service. In this paper, the authors are presenting the results of a systematic crack propagation analysis campaign performed on a compressor-blade-like structure. The point of novelty is that different blade design parameters are varied and explored in order to investigate how the crack propagation rate in low cycle fatigue (LCF, at R ratio R = 0) could be reduced. The design parameters/variables studied in this work are: (1) The length of the contact surfaces between the dovetail root and the disc and (2) their inclination angle (denoted as “flank angle” in the aero-engine industry). Effects of the friction coefficient between the disc and the blade root have also been investigated. The LCF crack propagation analyses have been performed by recalculating the stress field as a function of the crack propagation by using the FRacture ANalysis Code (Franc3D®).


2013 ◽  
Vol 747-748 ◽  
pp. 564-568 ◽  
Author(s):  
Dong Ye Yang ◽  
Wen Yong Xu ◽  
Zhou Li ◽  
Guo Qing Zhang ◽  
Zhing Liang Ning ◽  
...  

Low-cycle fatigue (LCF) fracture of the spray formed GH738 alloy was investigated under total strain controlled mode at 650°C. Basic theory for evaluating fatigue lives by fatigue striations has been introduced. The crack length a and the crack propagation rate da/dN were measured and the curve of da/dN in crack propagation zone was obtained with Paris formula and tabulation trapezoidal formula, respectively. The size and symmetry of rapid fracture zone of fatigue were also studied. The results showed that the relationship of a and N was linear with tabulation trapezoidal formula, and the da/dN and a was conic with Paris formula. At last, quantitative analysis of fatigue fracture was also discussed.


1993 ◽  
Vol 60 (1) ◽  
pp. 85-92 ◽  
Author(s):  
B. S. Hockenhull ◽  
E. M. Kopalinsky ◽  
P. L. B. Oxley

The frictional force when a hard surface slides over a relatively soft one is explained as the force needed to push waves of plastically deformed material along the soft surface ahead of asperities on the hard one. Using plastic strain increments determined from the wave model and assuming that wear occurs as a result of low-cycle fatigue, predictions are made of wear which take account of the surface roughness and lubrication conditions and a comparison is made with experimental results. Metallographic results are given which support the assumption that low cycle fatigue is important in causing surface damage and hence wear. These results also show that ironing of the surface by the passage of waves leads to surface damage and wear. It is concluded that in future work account will have to be taken of both low-cycle fatigue and ironing in making wear predictions.


1970 ◽  
Vol 36 (287) ◽  
pp. 1045-1051
Author(s):  
Eiryo SHIRATORI ◽  
Shinichiro NISHI ◽  
Akio IIDA ◽  
Takeshi ICHIKAWA

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