Zr61Ti2Cu25Al12非晶态合金在四点弯曲加载模式下的弯曲弹性极限OA
Flexural elastic limit of Zr61Ti2Cu25Al12 amorphous alloy under four-point bending loading mode
按照当前金属材料弯曲性能测试标准中推荐的跨厚比设计Zr61Ti2Cu25Al12非晶态合金的弯曲试验,试样将发生大挠度弹性变形.经过推导证明,弯曲试样不发生大挠度弹性变形的跨厚比上限取决于材料的弹性应变极限,锆基非晶态合金的弹性应变极限为2%,在四点1/4弯曲模式下不发生大挠度弹性变形的跨厚比上限值为22.在保证小挠度变形的前提下,通过四点弯曲循环加载-卸载试验,Zr61Ti2Cu25Al12合金试样最外表层发生初始剪切变形所对应的弯曲屈服应力约为1 760 MPa,产生0.01%残余应变所对应的弯曲弹性极限σp0.01为2 040 MPa.
The bending test of Zr61Ti2Cu25Al12 amorphous alloy was designed according to the span-thickness ratio recommended in the current metal material bending performance test standard,and the specimen would undergo large deflection elastic deformation.It was proved that the upper limit of the span-to-thickness ratio of the bending specimen without large deflection elastic deformation depended on the elastic strain limit of the material.The elastic strain limit of the zirconium-based amorphous alloy was 2%,and the upper limit of the span-to-thickness ratio without large deflection elastic deformation in the four-point 1/4 bending mode was 22.Under the premise of ensuring small deflection deformation,through the four-point bending cyclic loading and unloading test,the bending yield stress corresponding to the initial shear deformation of the outermost surface of the Zr61Ti2Cu25Al12 alloy sample was about 1 760 MPa,and the bending elastic limit σp0.01 corresponding to 0.01%residual strain was 2 040 MPa.
沈勇;温井龙
中国科学院金属研究所,沈阳 110016
金属材料
非晶态合金四点弯曲弯曲弹性极限跨厚比大挠度弹性变形
amorphous alloyfour-point bendingbending elastic limitspan-thickness ratiolarge deflection elastic deformation
《理化检验-物理分册》 2024 (008)
23-30 / 8
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