Porosity of nickel nanopowder compacts consolidated by gas extrusion

M. Alymov
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Abstract

The method of hot gas extrusion differs from other methods of metal pressure treatment in that the processed material is subjected to intense plastic deformation by extrusion under conditions of high isostatic pressure of inert gas and heating in the area of plastic deformation. The method makes it possible to process powder materials, while inevitably there is a need to control mechanical properties by controlling porosity and pressure inside the pores. The paper presents a method for calculating the pressure inside the pores from the minimum size of the closed pore. The pore pressure was evaluated on materials obtained by the consolidation of nickel nanopowders by hot gas extrusion. Quantitative processing of the material cross-section view images obtained by scanning electron microscopy showed that the minimum pore size is 220 nm. The formula for calculating the pore pressure is derived from the formula for calculating the critical pore radius. It takes into account the external impact pressure (the gas pressure during the extrusion process was equal to 400 MPa), the surface tension coefficient and the yield strength of nickel (at the extrusion start temperature of 910 °С), as well as the minimum pore radius. The proposed method for calculating the pressure inside a closed pore will allow us to evaluate the mechanical properties of materials obtained by various methods of powder metallurgy.
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气体挤压固结纳米镍粉末的孔隙率
热气体挤压法与其他金属压力处理方法的不同之处在于,被加工的材料在惰性气体的高等静压和塑性变形区加热的条件下,通过挤压而受到强烈的塑性变形。该方法使加工粉末材料成为可能,但不可避免地需要通过控制孔隙率和孔隙内压力来控制机械性能。本文提出了一种从封闭孔的最小尺寸出发计算孔内压力的方法。研究了高温气体挤压法制备的纳米镍粉末固结材料的孔隙压力。通过扫描电镜对材料横截面图像进行定量处理,发现最小孔径为220 nm。由临界孔隙半径计算公式推导出孔隙压力计算公式。考虑了外部冲击压力(挤压过程中气体压力为400 MPa)、镍的表面张力系数和屈服强度(挤压起始温度为910°С)以及最小孔隙半径。所提出的计算封闭孔内压力的方法将使我们能够评价通过各种粉末冶金方法获得的材料的力学性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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