scholarly journals On the diversity in design for different bending fretting fatigue mechanism

2019 ◽  
Vol 1 (9) ◽  
Author(s):  
Quazi Md. Zobaer Shah ◽  
Md. Asaduzzaman Chowdhury ◽  
Md. Arefin Kowser
2014 ◽  
Vol 85 (5) ◽  
pp. 055106 ◽  
Author(s):  
Xin Li ◽  
Zhengxing Zuo ◽  
Wenjie Qin

Author(s):  
Dong Ning ◽  
Min Zhang ◽  
Yongchen Xie ◽  
Yinbiao He ◽  
Weida Yao

In this paper, from the point of view of study and analysis on fretting wear and fretting fatigue mechanism of materials, the main differences between fretting fatigue and ordinary fatigue are summarized; further more, the damage reasons on a component in a NPP are analyzed and semi-quantitative relationship between fretting fatigue and ordinary fatigue for the component material is obtained to provide with referenced basis for structural improvement and failure analysis on original structure.


Author(s):  
Xin Li ◽  
Zhengxing Zuo ◽  
Wenjie Qin

Fretting fatigue is one of the typical failure forms of engine block. The aim of this study is to investigate the fretting fatigue mechanism of the V type engine and guide engine design. An experiential system was developed to simulate fretting fatigue failure under typical engine working condition. And a submodel was used in the finite element calculation to analyze contact status and stress distribution of the structural model. Through the fretting fatigue experimental observations and finite element analysis, it can be concluded that the additional rotate torque caused by bearing load and the bolt pretension load are the two main factors which affect the fretting fatigue mechanism of the V type engine. Appropriate increasing of the bolt pretension load and using extended skirt block with cross-bolted main bearings design will restrain the oscillation of the main bearing cap can be beneficial to fretting fatigue lives of the engine block.


Author(s):  
Kunio Asai ◽  
Shuichi Ishizawa ◽  
Nobuhiro Isobe

High velocity oxygen fuel (HVOF) sprayed stellite coating is often adopted on contact surfaces of the shrouds and stubs of titanium turbine blades, in order to increase fretting fatigue strength and reduce fretting wear. To confirm the effectiveness of the sprayed stellite coating, we conducted friction-type fretting tests originally developed to simulate the load condition of shrouds and stubs, vibratory force was carried only by friction force. We also investigated the fretting fatigue mechanism of coated materials by observing non-propagating cracks in the tested specimens and analyzed crack propagation behavior at the interface using fracture mechanics. The fretting fatigue tests confirmed that the sprayed stellite coating could double the fretting fatigue strength of Ti-6A1-4V. The fretting fatigue mechanism of Ti-6A1-4V with a sprayed stellite coating was revealed as follows: Final fracture was led by a newly initiated micro-crack at the interface as cracks initiated on the coating surface did not continuously propagate into the substrate but mainly propagated along the interface. The micro-crack propagation at the substrate depends on the length of interface crack. The longer interface crack delays micro-crack propagation to the substrate because the lines of force are less concentrated at the crack tip. Hence, the interface crack makes the fretting fatigue strength of coated Ti-6A1-4V higher than that of uncoated specimens. This finding was supported by the cross-sectional observations of non-propagating cracks in the tested specimens, and by FE analysis which revealed that ΔK of the substrate crack initiated at the interface decreases with an increase in delaminated crack length. Ti-6A1-4V with a sprayed stellite coating offers better wear resistance than uncoated Ti-6A1-4V because the coating’s friction coefficient is lower than that of Ti-6Al-4V, although the wear rates of coated and uncoated materials against the consumption energy per cycle were almost the same.


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