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Failure analysis of a truck diesel engine crankshaft

机译:卡车柴油发动机曲轴的故障分析

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A truck engine crankshaft fractured during the service. The fracture occurred on the crankshaft big-end on which the timing-gear and the flywheel flange were coupled and the fracture location was just situated at the assembling gap between them. The short cracks inclined at about 45 degrees to the shaft axis initiated from the surface of the crankshaft journal at the timing-gear side and mainly extended to the timing-gear side, leading to a zigzag cracking morphology on the journal surface. A complicated ratchet or star-shaped pattern of fracture typical of multiple fatigue cracks occurred on the fracture surface. The journal surface was locally induction-hardened. The surface hardness and the effective case depth on the hardened journal at the flywheel flange side corresponded to the specification. At the timing-gear side the surface hardness on the hardened journal was much lower than the specified lower limit and a low hardness region of 0.4 mm occurred on the most-surface of the hardened journal within which the hardness values were lower than the specified lower limit. The low surface hardness on the induction-hardened journal made fatigue resistance of the crankshaft decrease to lead to initiation and propagation of fatigue cracks in the weaker region. The assembling gap at which the fracture occurred was structure stress concentration site of the assembly constituted of the crankshaft, the timing-gear and the flywheel flange, equivalent to the deep notch. The excessive tightening of the timing-gear on the journal surface also contributed for the increasing of stress concentration. The fatigue crack origins were easy to initiate due to large stress concentration.
机译:在服务期间,卡车发动机曲轴破裂。裂缝发生在曲轴大端上,定时齿轮和飞轮法兰被耦合,并且裂缝位置恰好位于它们之间的组装差距。短裂缝倾斜于从正时齿轮侧从曲轴轴颈的表面发起的轴轴并且主要延伸到正时齿轮侧,导致轴颈表面上的锯齿裂解形貌。在裂缝表面上发生多重疲劳裂缝的复杂棘轮或星形图案。杂志表面是局部感应硬化的。在飞轮法兰侧的硬化轴上的表面硬度和有效壳体深度对应于该规范。在时刻齿轮侧,硬化轴颈上的表面硬度远低于指定的下限,并且在硬化轴颈的最大表面上发生0.4mm的低硬度区域,其中硬度值低于指定的下部限制。在诱导 - 硬化轴颈上的低表面硬度使曲轴的疲劳性降低降低,以导致疲软区域中的疲劳裂纹引发和繁殖。发生骨折的组装间隙是由曲轴构成的组件的结构应力集中位点,同时齿轮和飞轮法兰,相当于深凹口。在轴颈表面上的定时齿轮的过度紧张也有助于增加应力浓度。由于大应力浓度,疲劳裂缝起源易于启动。

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