改性对铝合金热膨胀的影响

Jan Novotný, Š. Michna, Martin Jaskevič, S. Legutko, I. Hren
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引用次数: 0

摘要

部件尺寸随温度变化的变化用一个称为热伸长率的量来描述。它是每种材料的基本特性之一,在为给定应用设计特定组件时,必须考虑到这一点。有时较高的热伸长率被认为是一种积极的性质,但在大多数应用中,随着温度的升高,人们努力降低热伸长率的幅度。不正确的设计可能导致部件失效或损坏。下面的研究包括两种最重要的铝亚共晶Al-Si合金,即AlSi7Mg0.3和AlSi7Mg0.6,用于汽车和航空航天工业。他们被选中是因为他们非常好的技术和机械性能。这些合金中的硅含量按重量计为5-3%。对合金进行分析,并测量其在-14 ~ 400℃温度范围内的伸长率曲线和组织形貌。为了进一步改善合金的组织、晶粒和性能,可以使用锶或AlSr10对合金进行改性,用AlTi5B1对钛进行接种,最后进行热处理硬化,然后将这些单独的处理结合起来。再次,将进行形态分析,以确定在个别处理后的结构变化,并测量处理合金在给定温度范围内的膨胀率,并测量热延伸系数。将获得的测量结果进行比较,以确定合金的适当处理是降低整体热延伸系数,还是在一定温度范围内降低热延伸系数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of modification of aluminum alloys on their thermal expansion
The change in the dimensions of a component with the change in temperature is described by a quantity called thermal elongation. It is one of the basic properties of every material and it is necessary to take it into account when designing a specific component for a given application. Sometimes higher thermal elongation is considered a positive property, but in most applications, there is an effort to reduce the magnitude of thermal elongation with increasing temperature. Incorrect design can result in component failure or destruction. The following research includes the two most important aluminum sub-eutectic Al-Si alloys, namely AlSi7Mg0.3 and AlSi7Mg0.6 used in the automotive and aerospace industries. They were chosen due to their very good technological and mechanical properties. The silicon content in these alloys is 5-3% by weight. The alloys will be analyzed and their elongation curves will be measured in the temperature range -14 to 400 oC and the morphology of the structure. To further improve the structure, grains and thus the resulting properties, the modification of alloys with strontium or AlSr10, titanium inoculation with AlTi5B1 and, last but not least, heat treatment hardening and subsequently a combination of these individual treatments will be used. Again, a morphological analysis will be performed to determine the changes in the structure after individual treatments and to measure the dilatation of the treated alloys in a given temperature range and to measure the coefficient of thermal elongation. The achieved measured results will be compared to determine the appropriate treatment of alloys to reduce the overall coefficient of thermal elongation, or to reduce the coefficient of thermal elongation for a certain temperature range.
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