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BULLETPROOF LIGHTWEIGHT METAL MATRIX MACROCOMPOSITES WITH CONTROLLED STRUCTURE AND MANUFACTURE THE SAME

机译:结构和制造均受控制的防弹轻质金属基复合材料

摘要

The lightweight bulletproof metal matrix macrocomposites (MMMC) contain (a) 10-99 vol. % of permeable skeleton structure of titanium, titanium aluminide, Ti-based alloys, and/or mixtures thereof infiltrated with low-melting metal selected from Al, Mg, or their alloys, and (b) 1-90 vol. % of ceramic and/or metal inserts positioned within said skeleton, whereby a normal projection area of each of said inserts is equal to or larger than the cross-section area of a bullet or a projectile body. The MMMC are manufactured as flat or solid-shaped, double-layer, or multi-layer articles containing the same inserts or different inserts in each layer, whereby insert projections of each layer cover spaces between inserts of the underlying layer. The infiltrated metal contains 1-70 wt. % of Al and Mg in the balance, optionally, alloyed with Ti, Si, Zr, Nb, V, as well as with 0-3 wt. % of TiB2, SiC, or Si3N4 sub-micron powders, to promote infiltrating and wetting by Al-containing alloys. The manufacture includes (a) forming the permeable metal powder and inserts into the skeleton-structured preform by positioning inserts in the powder followed by loose sintering in vacuum to provide the average porosity of 20-70%, (b) heating and infiltrating the porous preform with molten infiltrating metal for 10-40 min at 450-750° C., (c) hot isostatic pressing of the infiltrated composite, and (d) re-sintering or diffusion annealing. The positioning of the ceramic inserts in Ti-based powder is carried out by using a metal grid aiding the placement of inserts in a predetermined geometric pattern, and said grid becomes the integral part of the macrocomposite material. The technology is suitable for the manufacture of flat or shaped metal matrix macrocomposites having improved ductility and impact energy absorption such as lightweight bulletproof plates and sheets for airplane, helicopter, and automotive applications.
机译:轻质防弹金属基质大复合材料(MMMC)的体积为(a)10-99。钛,铝化钛,钛基合金和/或它们的混合物的渗透性骨架结构的百分比,渗透了选自Al,Mg或它们的合金的低熔点金属,以及(b)1-90 vol。 %的陶瓷和/或金属插入物位于所述骨架内,从而每个所述插入物的法向投影面积等于或大于子弹或弹体的横截面积。 MMMC被制造为扁平或实心的,双层或多层的制品,其在每一层中包含相同的插入物或不同的插入物,由此每层的插入物突出物覆盖下层的插入物之间的空间。渗透的金属含量为1-70wt。%。余量的Al和Mg,可选地与Ti,Si,Zr,Nb,V以及0-3 wt% TiB 2 ,SiC或Si 3 N 4 亚微米粉末的百分比,以促进含铝合金的浸润和润湿。制造包括(a)形成可渗透金属粉末,然后通过将插入物放置在粉末中,然后在真空中进行松散烧结,以提供20-70%的平均孔隙率,将其插入骨架结构的预成型坯中,(b)加热并渗透多孔用熔融的渗透金属在450-750℃下预成型10-40分钟。 C。,(c)渗透组合物的热等静压,和(d)再烧结或扩散退火。通过使用有助于以预定的几何图案放置插入物的金属栅格,将陶瓷插入物放置在Ti基粉末中,并且所述栅格成为大复合材料的组成部分。该技术适用于制造具有改善的延展性和冲击能量吸收能力的扁平或成形金属基质大复合材料,例如用于飞机,直升机和汽车应用的轻质防弹板和薄板。

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