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Heat-checking of hot work tool steels

机译:热工作工具钢的热检查

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Thermal fatigue (TF) is one of the life-limiting factors of the surface of the hot work tool steels. Bi-axial thermal strains and stresses are the main driving forces for the bi-axial cracking of tools well known as the heat checking. A TF rig using tubular specimens, induction heating and pressure air-cooling is developed. Two tempered martensitic steels 55NiCrMoV7 and X38CrMoV5 are investigated (47 HRC hardness) under a TF between 500-650°C. The effect of the specimen thickness on the softening (X38CrMoV5) is revealed by the post mortem room temperature microhardness measurements, X-ray residual stress and width broadening evaluations. The initial compressive residual stresses (due to the machining) become tensile very early under TF cycling. The X-ray width decreases with the number of thermal cycle. Cyclic inelastic straining and cyclic temperature tempering explain this softening. Cracking seems start when the oxide scale achieves a 《critical thickness》. Depending on the thermomechanical stress-state, the damage feature changes from a parallel multi-cracking near the extremities of the specimens (uni-axial loading) to a "cell-type" (or "square-type") cracking at the centre of the specimens (bi-axial loading). Uni-axial cracks can be very much extended. Under TF cycling, secondary cracks initiate progressively perpendicular to major axis of the uni-axial cracks. By increasing the longitudinal over the hoop stress ratio from the extremities (R=σzz/σθθ)=O) to the centre (R≈1), the density of the secondary cracks enhances. The 55NiCrMoV7 steel presents a lower heat checking resistance. In X38CrMoV5 the localised heat checking and the oxide-scale spalling are observed while in 55NiCrMoV7 the heat checking covers well the whole surface of the TF specimen. Oxidation-TF interactions play an important role in crack initiation and propagation.
机译:热疲劳(TF)是热工作工具钢表面的寿命限制因素之一。双轴热菌株和应力是用于良好称为热检查的工具的双轴破裂的主要驱动力。开发了使用管状试样,感应加热和压力空气冷却的TFIT。在500-650℃之间的Tf下调查(47 HRC硬度),在500-650°C之间进行调查(47小时硬度)。试验室温微硬度测量,X射线残留应力和宽度扩大评估,揭示了试样厚度对软化(X38Crmov5)的影响。初始压缩残余应力(由于机械加工)在TF循环下很早变得抗拉塞。 X射线宽度随着热循环的数量而减小。循环无弹性紧张和循环温度回火解释这种软化。当氧化物尺度达到“临界厚度”时,裂缝似乎开始。根据热机械应力 - 状态,损坏特征从标本(单轴负载)的四肢附近的并联多裂解变为“细胞型”(或“平方型”)在中心开裂标本(双轴负载)。单轴裂缝可能非常延伸。在TF循环下,次级裂缝逐渐发起垂直于单轴裂缝的主轴。通过从末端(R =ΣZZ/Σθθ)= O)向中心(R≈1)来增加纵向旋转应力比,次级裂纹的密度增强。 55nicrmov7钢呈较低的热检查阻力。在X38Crmov5中,在55 ritrmov7中观察到局部散热检查和氧化物级剥落,热检查覆盖TF样本的整个表面。氧化-TF相互作用在裂纹启动和繁殖中发挥着重要作用。

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