TiB<sub>2</sub>/A356复合材料航空零件的熔模铸造

张洁; 张东启; 武鹏伟; 王刚

doi:10.15980/j.tzzz.2012.10.019

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TiB₂/A356复合材料航空零件的熔模铸造
Investment Casting of Aeronautical Parts with A356/TiB₂ Aluminum Matrix Composite
2012年32卷第10期页码：925-927
纸质出版日期： 2012 ，
DOI： 10.15980/j.tzzz.2012.10.019

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[1]张洁,张东启,武鹏伟,王刚.TiB_2/A356复合材料航空零件的熔模铸造[J].特种铸造及有色合金,2012,32(10):925-927.

Zhang Jie, Zhang Dongqi, Wu Pengwei, et al. Investment Casting of Aeronautical Parts with A356/TiB₂ Aluminum Matrix Composite[J]. Special Casting & Nonferrous Alloys, 2012,32(10):925-927.
[1]张洁,张东启,武鹏伟,王刚.TiB_2/A356复合材料航空零件的熔模铸造[J].特种铸造及有色合金,2012,32(10):925-927. DOI： 10.15980/j.tzzz.2012.10.019.

Zhang Jie, Zhang Dongqi, Wu Pengwei, et al. Investment Casting of Aeronautical Parts with A356/TiB₂ Aluminum Matrix Composite[J]. Special Casting & Nonferrous Alloys, 2012,32(10):925-927. DOI： 10.15980/j.tzzz.2012.10.019.

摘要

研究了TiB2/A356复合材料的各热物性参数与TiB2体积分数的关系

并对ProCAST软件的数据库进行二次开发

以得到不同TiB2体积分数的TiB2/A356复合材料的热物性参数随温度变化的关系。对某航空零件进行熔模铸造的模拟和试验。结果表明

通过提高浇注温度、浇注速度以及添加保温材料

消除了该零件表面的缩松、缩孔缺陷。

Abstract

The relationship between the thermal-physical parameters of TiB2/A356 aluminum matrix composite and the volume fraction of TiB2 was investigated.Based on the secondary development of ProCAST software

the relationship between temperature change and thermal-physical parameters of TiB2/A356Al aluminum matrix composite with varied volumetric fraction of TiB2 was presented.A investment casting aeronautical part was simulated and produced.The results reveal that through increasing the pouring temperature and velocity of alloy melt as well as adding insulation materials around the shell mold

shrinkage porosity and shrinkage hole in the surface of the parts can be eliminated effectively.