Fig. 5 presents the SEM micrographs of original substrate and the HZ o的简体中文翻译

Fig. 5 presents the SEM micrographs

Fig. 5 presents the SEM micrographs of original substrate and the HZ obtained by LTH with different parameters. The element contents of P1-P3 detected by EDS are listed in Table 3. The microstructure of original substrate was tempered sorbite which was composed of whiteblocky ferrite with a smooth grain boundary and a great number of spheroidal carbide particles dispersed on boundary of the ferrite. For the laser transformation hardened samples, the microstructure was composed of uniform martensite with distinct boundary. However,there were no pores observed, while some cracks and other defects can be found. It was worth noting that the microstructure in the HZ consisted of plate martensite (PM), lath martensite (LM), retained austenite (RA) and some carbide particles. The structure that possessed the morphological feature of lenticular shape but the slices did not parallel to each other and intersected into a certain angle (60° or 120°) [19] was identified as PM, while structure that had the morphological features of being nearly parallel, almost equal length and arranged in bunches[20,21] was LM. For the sample with 1.7 kW 3 mm/s (Fig. 5(c e)), the microstructure was uniform and fine with almost the same amount of PM and LM, and some blocky RA were distributed widely. However, many carbide particles could still be observed on the boundary of martensite as shown in Fig. 5(e), which illustrated that the temperature on the surface was not high enough with lower laser power (namely,lower heat input) to dissolve more carbides during the heating process.As a result, the carbon content in RA surrounded by martensite of the sample with 1.7 kW 3 mm/s only accounted for 1.2% (P1). As the laser power increased to 1.8 kW 3 mm/s (Fig. 5(f-h)), the microstructure was coarser obviously, the number of PM was increased while the blocky RA was reduced simultaneously, and almost no carbide particles could be observed on boundary of the martensite (Fig. 5(h)). This suggested that higher laser power led to higher heat input and thus higher surface temperature, which would improve the diffusing ability of carbon atoms. More carbon atoms dissolved into the austenite during the austenitizing process, but they could not diffuse out of the grains in time during the rapid cooling process, thus leading to the formation of high-carbon martensite in the end. Meanwhile, due to the higherhardening temperature, the coarse martensite which transformed earlier bounded more austenite and prevented them from expanding and transforming into BCC structures, resulting in an increasing in number of RA surrounded by martensite at room temperature. Therefore, the carbon content in RA surrounded by martensite of the sample with 1.8 kW 3 mm/s was as high as 1.8% (P2), and more alloying elements such as Cr had been dissolved. For the sample with 1.8 kW 4 mm/s(Fig. 5(i–k)), due to the higher laser power, carbide particles couldhardly be found (Fig. 5(k)) as same as the sample with 1.8 kW 3 mm/s,and the blocky RA was less than the sample with 1.7 kW 3 mm/s.However, the lowest liner energy made it consist of more LM but less PM, this was because faster scanning velocity led to shorter interactiontime and faster cooling rate, some of carbon atoms had not yet dissolved into austenite before the process entering the cooling stage, so the carbon content in its RA surrounded by martensite was 1.5% (P3).
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Fig. 5 presents the SEM micrographs of original substrate and the HZ obtained by LTH with different parameters. The element contents of P1-P3 detected by EDS are listed in Table 3. The microstructure of original substrate was tempered sorbite which was composed of white<br>blocky ferrite with a smooth grain boundary and a great number of spheroidal carbide particles dispersed on boundary of the ferrite. For the laser transformation hardened samples, the microstructure was composed of uniform martensite with distinct boundary. However,there were no pores observed, while some cracks and other defects can be found. It was worth noting that the microstructure in the HZ consisted of plate martensite (PM), lath martensite (LM), retained austenite (RA) and some carbide particles. The structure that possessed the morphological feature of lenticular shape but the slices did not parallel to each other and intersected into a certain angle (60° or 120°) [19] was identified as PM, while structure that had the morphological features of being nearly parallel, almost equal length and arranged in bunches[20,21] was LM. For the sample with 1.7 kW 3 mm/s (Fig. 5(c e)), the microstructure was uniform and fine with almost the same amount of PM and LM, and some blocky RA were distributed widely. However, many carbide particles could still be observed on the boundary of martensite as shown in Fig. 5(e), which illustrated that the temperature on the surface was not high enough with lower laser power (namely,lower heat input) to dissolve more carbides during the heating process.As a result, the carbon content in RA surrounded by martensite of the sample with 1.7 kW 3 mm/s only accounted for 1.2% (P1). As the laser power increased to 1.8 kW 3 mm/s (Fig. 5(f-h)), the microstructure was coarser obviously, the number of PM was increased while the blocky RA was reduced simultaneously, and almost no carbide particles could be observed on boundary of the martensite (Fig. 5(h)). This suggested that higher laser power led to higher heat input and thus higher surface temperature, which would improve the diffusing ability of carbon atoms. More carbon atoms dissolved into the austenite during the austenitizing process, but they could not diffuse out of the grains in time during the rapid cooling process, thus leading to the formation of high-carbon martensite in the end. Meanwhile, due to the higher<br>在硬化温度下,较早转变的粗马氏体会束缚更多的奥氏体,并阻止其膨胀并转变为BCC结构,从而导致室温下马氏体包围的RA数量增加。因此,样品以1.8 kW 3 mm / s的马氏体包围的RA中的碳含量高达1.8%(P2),并且已溶解了更多的合金元素,例如Cr。对于1.8 kW 4 mm / s的样品(图5(i–k)),由于激光功率较高,因此<br>与1.8 kW的样品相同,几乎找不到碳化物颗粒(图5(k))。 3 mm / s,并且块状RA小于1.7 kW 3 mm / s的样品。然而,最低的衬里能量使其包含更多的LM,但PM更少,这是因为更快的扫描速度导致较短的相互作用<br>时间和更快的冷却速度,在进入冷却阶段之前,一些碳原子尚未溶解到奥氏体中,因此其RA中被马氏体包围的碳含量为1.5%(P3)。
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图5 以不同的参数呈现原始基板和 LTH 获得的 HZ 的 SEM 显微图。EDS 检测到的 P1-P3 元素内容列在表 3 中。原始基材的微结构由白色组成的钢化冰石<br>块状铁氧体与光滑的谷物边界和大量的球形硬质合金颗粒分散在铁氧体的边界。对于激光变换硬化样品,微结构由具有明显边界的均匀马腾石组成。然而,没有发现毛孔,而一些裂缝和其他缺陷可以发现。值得注意的是,HZ 中的微观结构包括板马腾石 (PM)、车床马腾石 (LM)、保留的奥斯汀石 (RA) 和一些硬质合金颗粒。具有透镜形状的形态特征,但切片彼此不平行,并相交成一定角度(60°或120°)[19]的结构被确定为PM,而具有几乎平行、几乎相等的长度和排列成束[20,21]的形态特征的结构为LM。对于1.7 kW 3 mm/s(图5(c e))的样品,微结构是均匀和精细的,PM和LM量几乎相同,一些块状RA分布广泛。然而,如图5(e)所示,许多碳化物颗粒仍能在马腾石的边界上观察到,这表明表面温度不够高,激光功率较低(即低热输入),在加热过程中溶解更多的碳化物。因此,以1.7 kW 3 mm/s为样本的马腾石包围的RA中的碳含量仅占1.2%(P1)。随着激光功率增加到1.8 kW 3 mm/s(图5(f-h),微结构明显变粗,PM数量增加,同时块状RA同时减少,在马腾锡(图5(h)边界上几乎无法观测到碳化物颗粒。这表明激光功率越高,热量投入越高,表面温度越高,碳原子的扩散能力就越强。更多的碳原子在沉降过程中溶解到沉降过程中,但它们不能在快速冷却过程中及时扩散出颗粒,最终导致高碳马腾石的形成。同时,由于较高<br>变硬的温度,粗糙的马腾石,改变了早期边界更多的奥斯汀,并阻止他们扩大和转化为BCC结构,导致在室温下被马腾石包围的RA数量增加。因此,以1.8千瓦3 mm/s为样品的马腾石包围的RA碳含量高达1.8%(P2),Cr等更多合金元素已被溶解。对于 1.8 kW 4 mm/s(图 5 (i-k) 的样品,由于激光功率较高,碳化物颗粒可以<br>几乎找不到(图5(k)与1.8千瓦样品相同
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图5显示了原始基板的SEM显微照片和不同参数下LTH获得的HZ。EDS检测P1-P3元素含量见表3。原始基体组织为回火索氏体,组织为白色<br>块状铁素体,晶界光滑,大量的球状碳化物颗粒弥散在铁素体的晶界上。激光相变硬化试样的显微组织为均匀的马氏体组织,边界清晰。但是,没有观察到气孔,同时可以发现一些裂纹和其他缺陷。值得注意的是,HZ的显微组织由板状马氏体(PM)、板条马氏体(LM)、残余奥氏体(RA)和一些碳化物颗粒组成。具有透镜状形态特征但切片不平行并相交成一定角度(60°或120°)[19]的结构被鉴定为PM,而具有近似平行、几乎等长、成束排列[20,21]的形态特征的结构被鉴定为LM。对于1.7 kW 3 mm/s的样品(图5(c e)),显微组织均匀且精细,PM和LM的含量几乎相同,并且一些块状RA分布广泛。然而,如图5(e)所示,在马氏体的边界上仍然可以观察到许多碳化物颗粒,这说明在较低的激光功率(即较低的热输入)下,表面温度不足以溶解更多的碳化物过程。作为结果是,1.7kw3mm/s试样中马氏体包围的RA中碳含量仅占1.2%(P1)。当激光功率增加到1.8kw3mm/s时(图5(f-h)),显微组织明显粗化,粉末数量增加,块状RA减少,马氏体边界几乎没有观察到碳化物颗粒(图5(h))。这表明激光功率越高,热输入越大,表面温度越高,碳原子的扩散能力越强。在奥氏体化过程中,更多的碳原子溶解在奥氏体中,但在快速冷却过程中,碳原子不能及时扩散出晶粒,最终形成高碳马氏体。同时,由于<br>硬化温度下,早期转变的粗马氏体结合更多的奥氏体,阻止其膨胀转变为体心立方结构,导致室温下被马氏体包围的RA数量增加。因此,1.8kw3mm/s试样马氏体包围的RA中碳含量高达1.8%(P2),Cr等合金元素被溶解。对于1.8 kW 4 mm/s的样品(图5(i–k)),由于较高的激光功率,碳化物颗粒可能<br>很难发现(图5(k))与1.8 kW 3 mm/s的样品相同,块状RA小于1.7 kW 3 mm/s的样品。然而,最低的线性能量使其由更多的LM组成,但较少的PM,这是因为更快的扫描速度导致更短的相互作用<br>随着冷却时间的延长和冷却速度的加快,在进入冷却阶段之前,部分碳原子还没有溶解到奥氏体中,因此被马氏体包围的RA中的碳含量为1.5%(P3)。<br>
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