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Material properties of normal and high strength aluminium alloys at elevated temperatures

机译:普通和高强度铝合金在高温下的材料性能

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Aluminium alloys are being used widely in multiple engineering applications. However, the material properties of aluminium alloys could change significantly at high temperatures. This paper studied the mechanical properties of normal strength aluminium alloy 6063-T5 and high strength aluminium alloy 6061-T6 at elevated temperatures. Tensile tests were conducted at room temperature (24 degrees C) and high temperatures up to 600 degrees C. Both steady temperature state tests and transient temperature state tests were used. The yield stress (i.e., 0.2% proof stress), the ultimate stress, the Young's modulus, and the ultimate strain were determined from tests. The measured material properties at different temperatures are compared with the predictions by the American and European specifications. A series of unified equations for calculating the reduction factors of the material properties at high temperatures are proposed herein; they are found to yield more accurate reduction factors for aluminium alloys.
机译:铝合金被广泛用于多种工程应用中。但是,铝合金的材料性能在高温下可能会发生显着变化。本文研究了普通强度铝合金6063-T5和高强度铝合金6061-T6在高温下的力学性能。拉伸试验在室温(24摄氏度)和高达600摄氏度的高温下进行。均使用了稳态温度测试和瞬态温度状态测试。由试验确定屈服应力(即0.2%屈服应力),极限应力,杨氏模量和极限应变。将在不同温度下测得的材料性能与美国和欧洲规范的预测值进行比较。本文提出了一系列用于计算高温下材料性能的折减系数的统一方程。发现它们可以产生更精确的铝合金还原系数。

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