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仿鸡脖子刚柔耦合结构的仿生机理及大变形建模

BIONIC MECHANISM AND LARGE-DEFORMATION MODELING OF RIGID-FLEXIBLE COUPLING STRUCTURE INSPIRED BY CHICKEN NECK

  • 摘要: 观察表明, 禽类颈部普遍具有刚柔耦合的特点, 在运动过程中, 可以辅助身体运动, 使得头部产生大变形. 在机器人、航空航天等领域普遍需要具有大变形、变刚度等特征的结构实现相关功能. 受禽类脖子结构的启发, 提出了一种仿鸡脖子刚柔耦合结构, 阐明仿鸡脖子的仿生机理并建立大变形模型. 首先, 从鸡颈部的生物解剖出发, 发现仿鸡脖子结构势必具有多自由度刚柔耦合的特征, 因此, 根据鸡脖子骨骼的构型构造出单节仿生标准单元, 根据肌肉的连接方式厘清节间弹性连接, 建立起仿鸡脖子刚柔耦合结构的力学模型; 然后, 通过定义连接矩阵描述节间弹性元件的分布和作用, 由此得到任意运动下的标准单元的力平衡方程; 最后, 选取了几种具有代表性的工况, 通过有限元分析验证理论建模方法的准确性并展示结构的非线性变刚度特征;在4种典型平面弯曲工况下得到不同变形与发力肌肉群的对应关系. 文章提出的仿鸡脖子刚柔耦合结构建模具有仿生机理清晰、适合大变形计算及结构具有非线性刚度特征等特点, 也解释了禽类颈部变形机理.

     

    Abstract: It is observed that the necks of birds generally have the characteristics of rigid-flexible coupling and variable stiffness, which can cause large head deformation with the body movement when the bird moves as walking or flighting. In the fields such as robotics and aerospace, structures with the characteristics of large deformation, variable stiffness and rigid-flexible coupling are generally required to achieve relevant functions. Inspired by the structure of the bird neck, this paper proposes a kind of rigid-flexible coupling structure imitating the chicken neck which clarifies its bionic mechanism, and establishes the mechanical model for flexible large deformations. Firstly, it discovers that bionic structure must have the characteristics of high-degree of freedom and rigid-flexible coupling based on the biological anatomical structure of the chicken neck. A bionic single standard unit is constructed according to the characteristics of the chicken neck skeleton and a model of spring connection between nodes is constructed according to the connection mode of muscles, thus a bionic rigid-flexible coupling structure is established by combining these two elements. Then, this paper describes the distribution and function of the elastic elements between nodes by defining the connectivity matrix, with which the force balance equation of any standard rigid section under any movement is obtained. Finally, several representative working conditions are selected for simulation, which verifies the accuracy of the established theoretical modeling method by the comparation with finite element analysis, and the nonlinear variable stiffness characteristics of the structure are displayed; The relations between deformations under four typical plane bending conditions and corresponding muscles force generation are obtained. The analysis on the bionic rigid-flexible coupling structure clearly shows the characteristics of bionic mechanism of chicken neck, which gives the theoretical calculation model for large deformations, representing the nonlinear stiffness characteristics. It also explains the deformation mechanism of the chicken neck.

     

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