高性能TiAl基复合材料内外“双层”耦合增强结构形成机制与优化调控
批准号:
52101034
项目类别:
青年科学基金项目(C类)
资助金额:
30.0 万元
负责人:
李明骜
依托单位:
学科分类:
金属材料制备与加工
结题年份:
2024
批准年份:
2021
项目状态:
已结题
项目参与者:
李明骜
中文摘要
TiAl基复合材料具有低密度、高比强度、优异的抗氧化性能和抗蠕变性能等优点,是替代镍基高温合金实现航空航天发动机大规模减重的首要候选材料。然而,TiAl基复合材料高温强度不足且室温塑性较差,难以满足航空航天工业对高温结构材料的性能要求。为解决上述瓶颈问题,本项目创新性地设计一种兼具内层增强结构(基体单元内部碳化物增强体弥散分布)与外层增强结构(基体单元界面层硼化物和碳化物呈准连续网状分布)的TiAl基复合材料,通过揭示B和C元素比例对TiAl基复合材料内、外“双层”增强结构演化的影响规律,建立基体单元及其界面层组织结构演化与材料力学性能的内在关联,阐明材料内、外“双层”耦合增强结构的形成机制,实现材料内、外“双层”耦合增强结构的优化调控,进而显著改善材料的室温塑性和高温强度,为发展高性能TiAl基复合材料制备新理论与新技术、推动TiAl基复合材料在航空航天领域的广泛应用奠定坚实基础。
英文摘要
TiAl matrix composites exhibit the advantages, such as low density, high specific strength, excellent oxidation and creep resistance, etc. Therefore, TiAl matrix composites become the preferred materials to replace nickel-based alloys and then achieve large-scale weight reduction of aerospace engines. However, due to the insufficient strength at high temperature and the poor plasticity at room temperature, TiAl matrix composites could not meet the requirements for high temperature structural materials in aerospace industry. In order to solve above bottleneck problems, this project innovatively designs a TiAl matrix composite, which consists of the inner reinforced structure (the dispersive distribution of carbides reinforcement in the matrix unit) and the outer reinforced structure (the borides and carbides distribute as quasi-continuous network in the interface layer of the matrix unit). This project would reveal the effect of boron and carbon elements ratio on the evolution of inner and outer "double layers" reinforced structure, establish the intrinsic relationship between matrix unit cooperating interface layer structure evolution and the mechanical properties, clarify the formation mechanism of the inner and outer "double layers" coupled reinforced structure, achieve the optimal regulation of the inner and outer "double layers" coupled reinforced structure, improve the plasticity at room temperature and the strength at high temperature of the materials. This project lays a solid foundation for the new theory and technology development of high performance TiAl matrix composites preparation and the wide application promotion of TiAl matrix composites in aerospace field.
本项目创新性地设计了一种兼具内层增强结构(基体单元内部碳化物增强体弥散分布)与外层增强结构(基体单元界面层硼化物和碳化物呈准连续网状分布)的TiAl基复合材料,明确了B和C元素比例对材料内外“双层”耦合增强结构演化的影响规律,建立了基体单元及其界面层组织结构演化与材料力学性能的内在关联,阐明了“双层”耦合增强结构的形成机制。研究结果表明,就“内层”弥散增强结构而言,C元素添加能够细化TiAl合金粉末微观组织的晶粒尺寸,促进α2相的形成和碳化物增强体的析出,提高TiAl合金粉末硬度;对于“外层”准连续网状增强结构而言,由于TiAl粉末和B4C粉末的原位自生反应,呈网状分布的针状和颗粒状增强体在TiAl基体单元界面层形成,分别为硼化物TiB相以及碳化物Ti2AlC和TiC相等,硼化物和碳化物增强体之间存在协同生长行为以及明显的晶体学位向关系,TiAl合金粉末与B4C粉末反应过程中TiB相会率先形核,随后TiC相以TiB相为基底在其表面台阶处形核,随着Ti和Al原子扩散取代TiC相中的C原子或空位,Ti2AlC相以TiC相为中间产物逐渐析出,最终TiB和Ti2AlC相协同生长构成基体单元界面层的准连续网状增强结构;随着B4C含量增加,准连续网状增强结构的连续性和厚度增加,相邻TiAl基体单元之间的连通性减弱;随着TiAl基体单元内部弥散增强结构及其界面层准连续网状增强结构的形成,内外“双层”耦合增强结构将TiAl基复合材料的室温延伸率和900℃的高温极限抗拉强度分别提升至1.42%和497.32MPa,此时,TiAl基体单元内C元素的含量为1.0at.%,界面层B4C的添加量为0.5wt.%。鉴于此,本项目制备出了兼具良好室温塑性和高温强度的TiAl基复合材料,为发展高性能TiAl基复合材料制备新理论与新技术、推动TiAl基复合材料在航空航天领域的广泛应用奠定了坚实基础。
低温瞬时液相烧结TiAl合金高致密化及微合金化机制研究
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项目类别:省市级项目
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资助金额:0.0万元
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批准年份:2025
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负责人:李明骜
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依托单位:
准连续网状增强TiAl基合金板材粉末冶金轧制变形机制多尺度研究
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批准号:--
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项目类别:省市级项目
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资助金额:0.0万元
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批准年份:2024
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负责人:李明骜
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依托单位:
国内基金
海外基金