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宽温域超弹性形状记忆合金设计优化研究进展

钱明芳,  尹钊,  王桂松,  张学习,  耿林

钱明芳,尹钊,王桂松,等. 宽温域超弹性形状记忆合金设计优化研究进展[J]. 北京航空航天大学学报,2026,52(10):3313-3328
引用本文: 钱明芳,尹钊,王桂松,等. 宽温域超弹性形状记忆合金设计优化研究进展[J]. 北京航空航天大学学报,2026,52(10):3313-3328
Qian M F,Yin Z,Wang G S,et al. Progress in design and optimization of wide-temperature-range superelastic shape memory alloys[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(10):3313-3328 (in Chinese)
Citation: Qian M F,Yin Z,Wang G S,et al. Progress in design and optimization of wide-temperature-range superelastic shape memory alloys[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(10):3313-3328 (in Chinese)

宽温域超弹性形状记忆合金设计优化研究进展

doi: 10.13700/j.bh.1001-5965.2025.0565
基金项目: 

国家重点研发计划(2022YFB3805701); 国家自然科学基金(52371182,51701052);黑龙江省自然科学基金(YQ2024E014);黑龙江省头雁创新团队项目

详细信息
    通讯作者:

    E-mail:xxzhang@hit.edu.cn

  • 中图分类号: TB31;TB34;TB381

Progress in design and optimization of wide-temperature-range superelastic shape memory alloys

Funds: 

National Key Research and Development Program of China (2022YFB3805701); National Natural Science Foundation of China (52371182,51701052); Heilongjiang Provincial Natural Science Foundation of China (YQ2024E014); Heilongjiang Touyan Innovation Team Program

More Information
  • 摘要:

    超弹性是形状记忆合金最重要的功能特性之一,其本质来源于应力诱导的可逆热弹性马氏体相变。超弹性温度窗口主要受合金化学成分与微观组织结构的协同影响。为此,系统回顾了近10年来具有宽温域超弹性特性的多类形状记忆合金体系的发展现状,重点比较了不同合金在超弹性温度窗口、可恢复应变大小及临界应力对温度的依赖性等关键性能参数方面的差异与特点。通过对比分析,为新型宽温域超弹性形状记忆合金的设计、制备与工程应用提供了理论支持与实践参考,并对该领域未来的发展方向进行了展望。

     

  • 图 1  温度-应力空间中形状记忆效应和超弹性区域示意图(根据文献[21]修正)

    Figure 1.  Schematic diagram of shape memory effect and superelastic region in temperature-stress space (modified based on Ref. [21])

    图 2  固溶态多晶合金在不同温度下的压缩应力-应变曲线

    Figure 2.  Compressive stress-strain curves of solid solution polycrystalline alloys at different temperatures

    图 3  不同合金的拉伸应力-应变曲线

    Figure 3.  Tensile stress-strain curves of different alloys

    图 4  DS-STG状态Ni50.8Ti49.2合金的制备工艺、性能、组织图[53]

    Figure 4.  Preparation process, properties, and microstructure of Ni50.8Ti49.2 alloy in DS-STG state[53]

    图 5  多晶Fe43.5Mn34Al15Ni7.5合金的拉伸应力-应变曲线[60]

    Figure 5.  Tensile stress-strain curves of polycrystalline Fe43.5Mn34Al15Ni7.5 alloy[60]

    图 6  Fe42Mn34Al13.5Cr3Ni7.5单晶的压缩应力-应变曲线[19]

    Figure 6.  Compression stress-strain curves of Fe42Mn34Al13.5Cr3Ni7.5 single crystal[19]

    图 7  [1 0 0]取向Fe43.5Mn34Al15Ni7.5单晶的超弹性响应及加载后的显微组织[64]

    Figure 7.  Superelastic response and post-loading microstructures of a [1 0 0]-oriented Fe43.5Mn34Al15Ni7.5 single crystal[64]

    图 8  Fe43.5Mn34Al15Ni7.5单晶沿不同晶向的压缩超弹性性能[66]

    Figure 8.  Compressive superelastic properties of Fe43.5Mn34Al15Ni7.5 single crystal along different crystal orientations[66]

    图 9  不同温度下合金的拉伸应力-应变曲线[8]

    Figure 9.  Tensile stress-strain curves of alloys at different temperatures[8]

    图 10  不同温度下合金的压缩应力-应变曲线

    Figure 10.  Compressive stress-strain curves of alloys at different temperatures

    表  1  宽温域超弹性Ni-Ti基SMA性能参数

    Table  1.   Performance parameters of wide temperature range superelastic Ni-Ti based SMA

    成分 超弹性温区/K 可逆应变/% $ \dfrac{\mathrm{d} \sigma_{\mathrm{c}}}{ \mathrm{d} T } \bigg/$(MPa·K−1) 加载方式 状态 参考文献
    Ni51.89Ti48.11 40~220 3.0~4.0 −8.77/2.11 压缩 S/STG [32]
    Ni51.8Ti48.2 40~180 2.0~2.5 −2.71/2.50 压缩 S/STG [33]
    Ni51.63Ti48.37 70~160 ~2.0 1.00 压缩 S/STG [32]
    Ni51.54Ti48.46 80~280 ~2.0 3.95 压缩 S/STG [32]
    Ni50.8Ti49.2 123~323 3.5~4.0 拉伸 CD/STG [16]
    Ni50.8Ti49.2 4.2~475 2.5~5.0 拉伸 CD/STG [47]
    Ni50.8Ti49.2 119~329 4.0~6.0 拉伸 CD/STG [51]
    Ni50.8Ti49.2 123~423 4.8~8.6 拉伸 CD/STG [53]
    Ni50.6Ti49.4 25~300 1.75~2.2 拉伸 NG/STG [17]
    Ni50Ti50 93~453 4.0~6.0 拉伸 CD/STG [52]
    Ti49.2Ni44.8Co6 123~223 ~4.0 3.17 拉伸 CD/NG [48]
    Ti47.6Ni42.4Cu10 70~200 ~1.5 −3.25/1.96 压缩 S [34]
    Ni49.4Ti48.1Sn2.5 113~298 3.6~5.0 压缩 S/STG [39]
    Ni49.4Ti47.6Sn3 83~298 ~5.5 压缩 S/STG [39]
    NiTiNb 77~333 ~5.0 −2.39/3.19 拉伸 CD/NG [49]
    Ni50.2Ti49.8/
    Ni46Ti47Nb3Fe4
    77~413 3.0~4.0 0.24/2.93 拉伸 CD/NG/CO [50]
     注:S表示固溶态,CD表示冷变形,NG表示纳米晶,CO表示复合材料。
    下载: 导出CSV

    表  2  宽温域超弹性Fe基SMA性能参数

    Table  2.   Performance parameters of wide temperature range superelastic Fe-based SMA

    成分 超弹性温区/K 可逆应变/% $\dfrac{\mathrm{d} \sigma_{\mathrm{c}}}{ \mathrm{d} T }\bigg/ $(MPa·K−1) 加载方式 状态 参考文献
    Fe43.5Mn34Al15Ni7.5 223~423 ~5.5 0.530 拉伸 PG [60]
    Fe42Mn34Al15Ni7.5Ti1.5 123~293 ~1.5 0.340 压缩 SG [61]
    Fe43.5Mn34Al15Ni7.5 10~300 ~1.3 0.510 压缩 SG [19]
    Fe42Mn34Al13.5Cr3Ni7.5 10~473 1.1~2.3 0.085 压缩 SG [19]
    Fe41Mn34Al12.5Cr5Ni7.5 10~300 1.2~1.4 −0.370 压缩 SG [19]
    Fe38Mn36Al11Cr7.5Ni7.5 10~293 ~1.2 −0.860 压缩 SG [19]
    Fe43.5Mn34Al15Ni7.5 193~433 1.7~2.0 0.540 拉伸 [1 0 0] SG [64]
    Fe43.5Mn34Al15Ni7.5 193~433 1.5~2.0 0.410 压缩 [1 0 0] SG [64]
    Fe43.5Mn34Al15Ni7.5 193~433 1.8~2.0 0.580 压缩 [1 2 3] SG [66]
    Fe68.8Pd31.2 240~350 0.6~3.7 压缩 [0 0 1] SG [69]
     注:PG表示多晶,SG表示单晶。
    下载: 导出CSV

    表  3  宽温域超弹性Cu基SMA性能参数

    Table  3.   Performance parameters of wide temperature range superelastic Cu-based SMAs

    成分 超弹性温区/K 可逆应变/% $\dfrac{\mathrm{d} \sigma_{\mathrm{c}}}{ \mathrm{d} T }\bigg/ $(MPa·K−1) 加载方式 状态 参考文献
    Cu70.6Al17.5Mn11.9 215~393 ~10.0 1.86 拉伸 CG [8]
    Cu68.8Al17.9Mn13.3 77~353 6.0~10.0 2.00 拉伸 CG [8]
    Cu68Al17Mn15 77~223 0.8~1.3 2.23 拉伸 BG [72]
    Cu68Al17Mn15 4.2~160 ~2.0 2.05 拉伸 SG [10]
    Cu71.1Al17.2Mn11.7 223~313 ~8.0 2.92 拉伸 BG [9]
     注:BG表示竹节晶织构,CG表示粗晶,SG表示单晶。
    下载: 导出CSV

    表  4  其他宽温域超弹性SMA性能参数

    Table  4.   Performance parameters of other wide temperature range superelastic SMA

    成分 超弹性温区/K 可逆应变/% $\dfrac{\mathrm{d} \sigma_{\mathrm{c}}}{ \mathrm{d} T }\bigg/ $(MPa·K−1) 加载方式 状态 参考文献
    Ni45Co5Mn36In14 4.2~200 ~2.0 −0.83 压缩 SG [74]
    Co51Cr27Ga11Si11 198~298 ~3.5 −3.18 压缩 SG [75]
    Co55.7Cr23.3Al10.5Si10.5 198~423 ~2.5 −1.12/1.09 压缩 [0 0 1] SG [76]
    Ni35Co20Fe18Ga27 123~423 ~11.0 拉伸 SG [77]
    Mg78.7Sc21.3 123~298 ~1.0 拉伸 STG [14]
    Ti75.25Al20Cr4.75 4.2~400 ~5.7 −2.13/2.49 拉伸 SG [78]
     注:SG表示单晶。
    下载: 导出CSV
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出版历程
  • 收稿日期:  2025-08-13
  • 录用日期:  2025-10-24
  • 网络出版日期:  2025-10-30
  • 整期出版日期:  2026-10-01

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