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| 1 | Bio-inspired polygonal skeleton structure for vibration isolation:Design,modelling,and experiment显示文摘Inspired by the safe landing of a cat falling from a high altitude,a bio-inspired polygonal skeleton(BIPS) structure is proposed,and its nonlinear characteristics are systematically studied to explore its potential application in the suppression of vibration. The polygon is formed by the skeleton structure of the cat’s entire body and the ground. The BIPS system consists of two symmetrical bionic legs with three robs(as skeleton) and four horizontal springs(as muscle). Two bionic legs are connected through the bearing platform(as spine),which could adjust the distance between the two bionic legs. A theoretical model is developed to characterize its stiffness nonlinearity through geometrical and mechanical analysis. Parameter analysis reveals that the BIPS structure has diverse stiffness,including nonlinear positive stiffness and negative stiffness. By imitating adjustment of leg posture and telescopic function of the spine(control the distance between legs),these flexible stiffness properties can be adjusted by structure parameters. In addition,the load capacity and working range can also be designed by the length of the bars,the initial angle,the mounting position,and the spring stiffness. The experimental setup is established,and the vibration isolation performance under various excitation is tested. The experimental results verify the accuracy of the dynamic model and also show that the proposed BIPS structure can suppress the vibration effectively under a variety of excitations. These peculiarities may provide potential possibility of an innovative approach to passive vibration control and isolation. | YAN Ge WANG Sen ZOU HongXiang ZHAO LinChuan GAO QiuHua ZHANG WenMing | 2020 | Science China(Technological Sciences)2020，63，12： | 5 |
| 2 | 基于结构声强法的机匣振动能量传递特性显示文摘为了分析在转子不平衡力激励作用下机匣上纵波、剪切波、扭转波以及弯曲波所携带的瞬态与稳态振动能量的分布规律和传递特性,将结构声强法拓展成矩阵的形式应用到航空发动机领域。建立了转子不平衡力作用下的双转子-支承-机匣耦合模型,通过由有限元工具和自编译程序组建的计算系统,求解并可视化了在高低压转子不平衡力激励作用下机匣瞬态与稳态的总结构声强场以及不同类型振动波的结构声强场。此外,通过运动方程推导并分析了结构声强与结构振动特性之间的内在物理关系。结果表明,机匣上纵波振动能量穿过法兰边后沿其周向传递,而剪切波和扭转波所携带的振动能量则可以穿过法兰边沿机匣轴向传递;支板上的振动能量首先以弯曲波的形式传递到机匣上,振动能量在机匣上沿主要路径传递过程中会发生不同类型振动波相互转换的现象;结构声强通过结构的动能变化率、应变能变化率以及阻尼耗散等能量参数与结构振动特性产生内在物理联系,对结构振动的控制本质上就是对振动能量流的控制。研究结论可为航空发动机机匣以及整机减振提供一定理论指导。 | 马英群 徐蒙 张锴 赵巍 赵庆军 | 2019 | 航空学报2019，40，9： | 0 |
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