目前以航空航天为代表的极端环境领域对板结构的静态和动态力学性质都提出了更高的要求。在保证结构承载能力的同时,还需要实现轻质化以及使其具有多频带减隔振功能。针对上述要求,设计了一种拉扭耦合超结构板,利用由两个自由度耦合谐...目前以航空航天为代表的极端环境领域对板结构的静态和动态力学性质都提出了更高的要求。在保证结构承载能力的同时,还需要实现轻质化以及使其具有多频带减隔振功能。针对上述要求,设计了一种拉扭耦合超结构板,利用由两个自由度耦合谐振产生的两个低频弯曲波带隙,实现超结构板的低频双频带减振。首先提出一种具有拉扭双自由度的单胞等效模型,并在此基础上利用平面波展开(Plane Wave Expansion,PWE)法进行超结构板带隙特性的计算,最后通过有限元分析(Finite Element Analysis,FEA)验证了带隙计算方法的正确性。研究发现,相比于拉压平动单自由度谐振子,拉扭耦合双自由度谐振子会在板结构中打开一个新的弯曲波带隙。进一步分析归一化等效刚度系数对两个带隙位置和带宽的影响。最后,利用有限元方法计算10'5阵列超结构板的振动传递率,得出的振动衰减区域与由理论计算所得的带隙位置一致。有关结论可为轻质超结构板的多频带减振设计提供参考。展开更多
The static test of 13 square hollow section(SHS) X-joints with different β and different types of plate reinforcement under in-plane moment in brace was carried out. Experimental test schemes, failure modes of specim...The static test of 13 square hollow section(SHS) X-joints with different β and different types of plate reinforcement under in-plane moment in brace was carried out. Experimental test schemes, failure modes of specimens, moment-vertical displacement curves, moment-deformation of the chord, and strain strength distribution curves were presented. The effect of β and plate reinforcement types on in-plane flexural property of SHS X-joints was studied. Results show that punching shear of chord face disappears, brace material fracture appears and concave and convex deformation of chord decrease when either collar plates or doubler plates were welded on chord face. Moment-vertical displacement curves of all specimens have obvious elastic, elastic-plastic and plastic stages. As β increases, the in-plane flexural ultimate capacity and initial stiffness of joints of the same plate reinforcement type increase, but ductility of joints decreases. With the same β, the in-plane flexural initial stiffness and ultimate capacity of doubler plate reinforced joints, collar plate reinforced joints, and unreinforced joints decrease progressively. Thickness of reinforcement plate has no obvious effect on in-plane flexural initial stiffness and ultimate capacity of joints. As thickness of reinforcement plate increases, the ductility of reinforced X-joints decreases. The concave and convex deformation of every specimen has good symmetry;as β increases, the yield and ultimate deformation of chord decrease.展开更多
文摘目前以航空航天为代表的极端环境领域对板结构的静态和动态力学性质都提出了更高的要求。在保证结构承载能力的同时,还需要实现轻质化以及使其具有多频带减隔振功能。针对上述要求,设计了一种拉扭耦合超结构板,利用由两个自由度耦合谐振产生的两个低频弯曲波带隙,实现超结构板的低频双频带减振。首先提出一种具有拉扭双自由度的单胞等效模型,并在此基础上利用平面波展开(Plane Wave Expansion,PWE)法进行超结构板带隙特性的计算,最后通过有限元分析(Finite Element Analysis,FEA)验证了带隙计算方法的正确性。研究发现,相比于拉压平动单自由度谐振子,拉扭耦合双自由度谐振子会在板结构中打开一个新的弯曲波带隙。进一步分析归一化等效刚度系数对两个带隙位置和带宽的影响。最后,利用有限元方法计算10'5阵列超结构板的振动传递率,得出的振动衰减区域与由理论计算所得的带隙位置一致。有关结论可为轻质超结构板的多频带减振设计提供参考。
基金Projects(51278209 and 51478047) supported by the National Natural Science Foundation of ChinaProject(ZQN-PY110) supported by Promotion Program for Young and Middle-aged Teacher in Science and Technology Research of Huaqiao University,China+1 种基金Project(2014FJ-NCET-ZR03) supported by Program for New Century Excellent Talents in Fujian Province University,ChinaProject(JA13005) supported by Incubation Programme for Excellent Young Science and Technology Talents in Fujian Province Universities,China
文摘The static test of 13 square hollow section(SHS) X-joints with different β and different types of plate reinforcement under in-plane moment in brace was carried out. Experimental test schemes, failure modes of specimens, moment-vertical displacement curves, moment-deformation of the chord, and strain strength distribution curves were presented. The effect of β and plate reinforcement types on in-plane flexural property of SHS X-joints was studied. Results show that punching shear of chord face disappears, brace material fracture appears and concave and convex deformation of chord decrease when either collar plates or doubler plates were welded on chord face. Moment-vertical displacement curves of all specimens have obvious elastic, elastic-plastic and plastic stages. As β increases, the in-plane flexural ultimate capacity and initial stiffness of joints of the same plate reinforcement type increase, but ductility of joints decreases. With the same β, the in-plane flexural initial stiffness and ultimate capacity of doubler plate reinforced joints, collar plate reinforced joints, and unreinforced joints decrease progressively. Thickness of reinforcement plate has no obvious effect on in-plane flexural initial stiffness and ultimate capacity of joints. As thickness of reinforcement plate increases, the ductility of reinforced X-joints decreases. The concave and convex deformation of every specimen has good symmetry;as β increases, the yield and ultimate deformation of chord decrease.
