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横向冲击载荷下伪弹性TiNi合金矩形悬臂梁结构响应的实验研究
引用本文:张兴华,唐志平,李丹,吴会民. 横向冲击载荷下伪弹性TiNi合金矩形悬臂梁结构响应的实验研究[J]. 实验力学, 2008, 23(1): 43-52
作者姓名:张兴华  唐志平  李丹  吴会民
作者单位:中国科学技术大学,中科院材料力学行为和设计重点实验室,合肥,230027
摘    要:利用改装的霍普金森压杆装置对伪弹性TiNi合金矩形截面悬臂梁进行了横向冲击实验研究.结果表明:冲击自由端时,只在根部附近产生一个相变铰,冲击梁中间某位置时,则可能在多处形成相变铰;相变铰形成时拉伸和压缩两侧应变存在一定的不对称性,但是差别并不明显;相变铰的形成与发展过程中,应变并不是单调增加的,而是带有波动性;卸载后相变铰消失,TiNi悬臂梁形状完全回复;自由振动前期,应变的平衡位置与挠度的平衡位置有一定偏离,并且这种偏离随着梁的振动逐渐减小直至消失.TiNi悬臂梁的冲击特性受热弹性马氏体相变和逆相变的支配,不同于传统的弹塑性机制.

关 键 词:冲击相变  TiNi悬臂梁  相变铰  形状记忆合金(SMA)  横向冲击  横向冲击载荷  伪弹性  TiNi  合金  矩形  悬臂梁  结构响应  实验  研究  Impact  Transversal  Cantilever  Rectangular  Alloy  Structural Response  Dynamic  Study  机制  弹塑性  逆相变
文章编号:1001-4888(2008)01-0043-10
收稿时间:2007-04-10
修稿时间:2008-12-09

Experimental Study of the Dynamic Structural Response of Pseudo-Elastic Ti-Ni Alloy Rectangular Cantilever Beam
ZHANG Xing-hua,TANG Zhi-ping,LI Dan,WU Hui-min. Experimental Study of the Dynamic Structural Response of Pseudo-Elastic Ti-Ni Alloy Rectangular Cantilever Beam[J]. Journal of Experimental Mechanics, 2008, 23(1): 43-52
Authors:ZHANG Xing-hua  TANG Zhi-ping  LI Dan  WU Hui-min
Affiliation:Key Lab for Mechanical Behavior and Design of Materials,CAS,University of Science and Technology of China,Hefei 230027,China;Key Lab for Mechanical Behavior and Design of Materials,CAS,University of Science and Technology of China,Hefei 230027,China;Key Lab for Mechanical Behavior and Design of Materials,CAS,University of Science and Technology of China,Hefei 230027,China;Key Lab for Mechanical Behavior and Design of Materials,CAS,University of Science and Technology of China,Hefei 230027,China
Abstract:Experimental investigation of pseudo-elastic Ti-Ni alloy cantilever beam with rectangular cross-section under a transversal impact loading was conducted by using a revised Hopkinson bar apparatus. It is found that only one transformation hinge (TH) formed near the fixed end of Ti-Ni cantilever beam when the impact is applied at the free end, while several THs may form at different locations when the impact is applied on the middle of the beam; TH displays asymmetry on the both tension and compression sides, but the difference is not obvious. During the period of formation and development of TH strain increases not monotonously but with fluctuation. TH has disappeared after unloading and the Ti-Ni beam has recovered its original shape. During the early stage of free vibration, there are some differences between the equilibrium position of strain and deflection, which has decreased and finally disappeared along with the vibration of Ti-Ni beam. The impact response of Ti-Ni cantilever beams is controlled by the thermo-elastic martensite phase transformation and inverse transformation, which differs from the conventional elastic-plastic mechanism.
Keywords:shock induced phase transition   Ti-Ni cantilever   transformation hinge   shape memory alloy(SMA)   transversal impact
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