为研究铝合金轴心受压构件的局部稳定性能,采用有限元软件ANSYS对132个十字形截面、144个箱形截面及180个工形截面进行数值分析。研究板件厚度、局部几何初始缺陷、整体几何初始缺陷、屈服强度、Ramberg—Osgood模型中应变硬化指数n的取值以及板件间相互作用对3类构件屈曲后性能的影响,给出板件全部有效的最大宽厚比b/t及有效厚度折减系数α1。分析结果表明:局部几何初始缺陷和屈服强度对b/t及α1影响较大,在工程实际中必须考虑;n值主要影响b/t,对α1的影响不大;板件厚度和整体几何初始缺陷对两者没有影响;工形截面翼缘和腹板间存在相互作用,使两者α1差值减小。在实际工程中,要控制板件的局部几何初始缺陷大小,至少为规范中的普通级;当材性未知时,可取n=f0.2/10,且在该值的±50%之内,n的取值对板件的有效厚度折减系数基本没有影响。
In order to study the local buckling behavior of aluminium alloy columns under unflorm compression, finite element analysis of 132 cruciform sections, 144 square-hollow sections and 180 1 sections are carried out by ANSYS. The influence of plate thickness, local initial geometric imperfections, overall initial geometric imperfections, yield strength, the value of strain-hardening exponent n from Ramberg-Osgood model and interaction between adjacent members are studied. The limiting width-thickness ratio [ b/t ] and reduction factor of effective thickness cq are given. The results show that local initial geometric imperfections and yield strength have a remarkable influence on [ b/t ] and c~t, which must be considered ; n effects mainly on [ b/t ] of reinforced plate and little on a~; plate thickness and overall initial geometric imperfections have no influence on both of them; interaction between flange and web of I sections makes the difference between reduction factor of them decrease. Therefore, local initial geometric imperfections must be limited; n can be taken as f0.2/10 if unknown and within ± 50% of this value, the value of n effects little on reduction factor of effective thickness.