Determination of step aging effective modes of a stamped alloy for hot deformation

V.Ya. Grabovsky, V. Kanyuka, O. Lysytsia
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Abstract

Using the method of mathematical planning of the experiment, the influence of two-stage (low-temperature + high-temperature) aging on the hardness and high-temperature (750 °C) impact strength of a stamped alloy ХН35ВТЮ (EK39) for hot pressing of metals was investigated. The need to increase the high-temperature impact strength of the alloy is a significant decrease (failure) with increasing test temperature from room temperature to 700… 750 °C. To isolate the particles of the reinforcing γ′-phase of the Ni3(Al,Ti) type during aging, the alloy was previously hardened in oil from a temperature of 1150 °C. Determination of the most effective modes of two-stage aging was performed using a small replica of the orthogonal plan of the second order type 24-1. The first (low-temperature) stage corresponds to the beginning of spinodal decay of supersaturated solid solution at the stage of formation of Guinness-Preston zones, and the second (high-temperature) - to the formation of particles of stable γ′-phase type Ni3(Ti,Al). Temperature and aging time on each step varied. According to the planning matrix, regression equations were calculated, and additional experiments were performed to determine the modes of step aging, which provide the alloy with a higher level of selected properties compared to the recommended single aging (780 °C, 10 hours). According to the obtained regression equations, the change in the aging temperature at the second stage of aging does not affect the hardness of the alloy within its variation (750 °C–800 °C). The effect on impact strength of changes in temperature (650 °C–700 °C) and holding time (2–6 hours) at the first stage of aging is also insignificant. According to the results of processing and analysis of experimental data, it is established that the increase of high-temperature impact strength from 38 to 120 J/cm2 (while maintaining hardness and high-temperature strength at the same level) is achieved after step aging 700 °C, 20 hours + 750 °C, 2 hours. The increase in hardness from 29 to 33 HRC with a simultaneous increase in impact strength to 55 J/cm2 provides step aging of 725 °C, 10 hours + 775 °C, 6 hours. According to the results of electron microscopic study of the microstructure, it was found that the achieved level of impact strength after step aging is provided by increasing the dispersion of spherical particles of the γ′-phase of the type Ni3(Al,Ti). The increase in hardness is due to a more uniform volume distribution and a smaller cross-sectional scatter of γ′-phase particles. Keywords: aging, dispersion hardening, impact strength, microstructure, stamping tool.
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热变形冲压合金阶跃时效有效模态的测定
采用实验数学规划的方法,研究了两阶段(低温+高温)时效对金属热压用冲压合金?Н35ВТ(EK39)硬度和高温(750°C)冲击强度的影响。随着试验温度从室温提高到700…750°C,提高合金高温冲击强度的需要显著降低(失效)。为了在时效过程中分离Ni3(Al,Ti)型增强γ′相的颗粒,该合金预先在1150°C的油中硬化。使用二阶类型24-1的正交计划的小复制品来确定两阶段老化的最有效模式。第一阶段(低温)对应于在Guinness Preston区形成阶段过饱和固溶体的旋节衰变的开始,第二阶段(高温)对应于稳定γ′相型Ni3(Ti,Al)颗粒的形成。每个步骤的温度和老化时间各不相同。根据规划矩阵,计算回归方程,并进行额外的实验来确定阶梯时效的模式,与推荐的单一时效(780°C,10小时)相比,阶梯时效为合金提供了更高水平的选定性能。根据获得的回归方程,第二阶段时效温度的变化在其变化范围内(750°C–800°C)不会影响合金的硬度。在老化的第一阶段,温度(650°C–700°C)和保温时间(2–6小时)的变化对冲击强度的影响也不显著。根据对实验数据的处理和分析结果,确定在700°C、20小时+750°C、2小时的步进时效后,高温冲击强度从38提高到120 J/cm2(同时保持硬度和高温强度在同一水平)。硬度从29 HRC增加到33 HRC,同时冲击强度增加到55 J/cm2,可提供725°C、10小时+775°C、6小时的阶跃老化。根据微观结构的电子显微镜研究结果,发现通过增加Ni3(Al,Ti)型γ′相球形颗粒的分散度,可以获得分级时效后达到的冲击强度水平。硬度的增加是由于γ′相颗粒的体积分布更均匀和横截面散射更小。关键词:时效,分散硬化,冲击强度,微观结构,冲压工具。
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审稿时长
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