一体化蜂窝结构纤维增强碳化硼 / 碳化硅复合装甲及其制备方法

By using an integrated honeycomb structure fiber-reinforced boron carbide/silicon carbide composite armor, the problem of insufficient resistance to multiple attacks and toughness of ceramic armor has been solved, achieving a high-strength, high-modulus interface bond and improving protective performance.

CN118031724BActive Publication Date: 2026-07-17HUNAN UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
HUNAN UNIV
Filing Date
2024-03-29
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing ceramic armor is insufficient in terms of resistance to multiple attacks and toughness, and its spliced ​​structure has shortcomings such as fragile gaps and uneven protective performance.

Method used

An integrated honeycomb structure fiber-reinforced boron carbide/silicon carbide composite armor is adopted. The fiber-reinforced silicon carbide honeycomb skeleton and fiber-reinforced boron carbide ceramic honeycomb filling material are formed by silicon infiltration reaction sintering, forming high-strength, high-modulus silicon carbide and boron carbide ceramic materials, achieving dense bonding at the interface.

Benefits of technology

It significantly improves the armor's ballistic performance and interfacial bonding strength, avoids the gap problem in spliced ​​structures, and provides a way to prepare high-performance ceramic armor.

✦ Generated by Eureka AI based on patent content.

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Abstract

提供了一种一体化蜂窝结构纤维增强碳化硼 / 碳化硅复合装甲及其制备方法,复合装甲包括经硅渗透反应烧结形成一体化结构的纤维增强碳化硅蜂窝骨架和纤维增强碳化硼陶瓷蜂窝填充材料,纤维增强碳化硅蜂窝骨架与纤维增强碳化硼陶瓷蜂窝填充材料的体积比范围为:1:(1.5‑5.5);产品的平均密度为2.4‑2.9g / cm3;本发明产品是在蜂窝骨架素坯和填充浆料填充成型的基础上,经高温炉液相硅渗透反应烧结获得一体化结构,获得的蜂窝骨架为高强高模高硬度的碳化硅陶瓷材料,具有非常好的抗弹效果,蜂窝填充材料也为高强高模高硬度的碳化硼 / 碳化硅陶瓷材料,同样具有优异的的抗弹性能。
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