热静态压的TiC/TC4复合材料的机械性能和断裂行为
Zhiyu Sun1,2, Jinyi Duan2, Xiang Wu2
1Cast Titanium Alloy R&D Center, Beijing Institute of Aeronautical Materials, Beijing 100095, China.
Materials (Basel, Switzerland)
|December 31, 2025
概括
热静态压缩 (HIP) 产生了强大的矩阵复合材料 (TMC),具有出色的高温性能. 这些TiC/TC4复合材料由于其增强的机械性能,具有航空航天应用的潜力.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 矩阵复合材料 (TMC) 由于其高强度和低密度,对航空航天至关重要.
- 传统的TMC造方法存在诸如分离和粗增强等缺陷.
- 需要改进的制造方法来增强TMC,以满足苛刻的应用.
研究的目的:
- 使用热静态压缩 (HIP) 制造TiC/TC4矩阵复合材料.
- 为了评估所制造的复合材料的室温和高温机械性能.
- 研究TiC/TC4复合材料的强化机制和断裂行为.
主要方法:
- 通过热同静压 (HIP) 制造TiC/TC4复合材料.
- 在室温和600°C的拉力测试.
- 塑料变形和断裂行为的微结构分析.
主要成果:
- C/TC4复合材料在室温下实现了1058±8 MPa的抗拉强度和958±12 MPa的屈服强度.
- 高温测试显示,在600°C时,拉伸强度约为500MPa.
- 断裂分析显示了室温和高温之间的裂启动差异,由粒子,固体溶液和负载传递机制加强.
结论:
- 热静态压缩 (HIP) 是生产高性能TiC/TC4矩阵复合材料的有效方法.
- 复合材料在室温和高温下表现出极好的机械性能.
- 了解增强机制和变形行为是优化TMCs用于航空航天应用的关键.
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