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Eddy-Current Testing of Fatigue Degradation in Additionally Heat-Treated Gas Powder Laser Clad NiCrBSi Coating under Contact Fatigue Loading

机译:抗疲劳降解的涡流试验在接触疲劳负荷下耐热处理的气体粉末激光粘土涂层

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The paper studies the applicability of eddy-current technique to testing fatigue degradation in Ni-18.2Cr-3.3B-4.2Si coating, produced by gas powder laser cladding and subjected to additional high-temperature annealing at 1025 °C, under contact loading. It is demonstrated that eddy-current testing of fatigue degradation inNi-18.2Cr-3.3B-4.2Si coating under contact loading after high-temperature annealing has certain limitations caused by the high brittleness of this coating. In this case, it is possible to test only a sharp increase in the sizes of contact damages, which occurs at 8×10~5 cycles under these loading conditions and results from the formation of a great number of peripheral ring cracks in the fracture zone; the eddy-current readings a decrease due to the increasing electrical resistivity of the coating. Testing can be performed by eddy-current measurements at high excitation frequencies of an eddy-current transducer (f=72-120 kHz), when the effect of the ferromagnetic steel base on the eddy-current readings a is minimum.
机译:本文研究了涡流技术的适用性,通过气体粉末激光包层制备的Ni-18.2Cr-3.3b-4.2SI涂层疲劳降解的适用性,并在接触载荷下进行1025℃的额外高温退火。结果表明,高温退火后,在接触载荷下,抗疲劳降解Inni-18.2Cr-3.3b-4.2SI涂层的涡流测试具有一定的局限性由该涂层的高脆性引起的限制。在这种情况下,可以仅测试接触损坏的尺寸的急剧增加,这在这些装载条件下发生在8×10〜5周期中,并由裂缝区中形成大量的外周环裂纹产生;由于涂层的电阻率增加,涡流读数降低。当铁磁钢基底在涡流读数A上的效果最小时,可以通过涡流换能器(F = 72-120 kHz)的高励磁频率下进行测试。

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