基于螺旋理论的Hexaglide型并联机构奇异性分析
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南京航空航天大学

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Singularity Analysis of a Hexaglide Parallel Mechanism Based on Screw Theory
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Nanjing University of Aeronautics and Astronautics

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    摘要:

    以Hexaglide型并联机构为研究对象,通过对并联机构的几何特性分析,得到每条支链的单位力旋量,结合并联机构的静力平衡条件,推导出该并联机构的一阶力影响系数矩阵,基于构造零列的方法使一阶力影响系数矩阵行列式奇异,进而确定了使该并联机构发生奇异的几何条件,并通过构造行、列线性相关性的方法推导出Hexaglide型并联机构不会发生构型奇异的条件,在此基础上,将三类奇异条件统一转化为参数化表达式,定义了可量化的几何安全距离指标,可带入优化模型用于设计阶段的奇异规避,为该机构的设计提供了理论支持和方法依据。

    Abstract:

    Taking the Hexaglide-type parallel mechanism as the research object, the unit wrench screw of each limb is obtained by analyzing the geometric characteristics of the mechanism, and the first-order force influence coefficient matrix is derived based on the static equilibrium conditions. Using a zero-column construction method, the determinant of this matrix is made singular, thereby identifying the geometric conditions under which the mechanism becomes singular. Furthermore, by constructing linear dependencies among rows and columns, the conditions under which the Hexaglide mechanism does not exhibit configuration singularity are derived. On this basis, the three types of singularity conditions are unified into a parametric form, and a quantifiable geometric safety distance index is defined, which can be incorporated into an optimization model for singularity avoidance at the design stage. This work provides theoretical support and a methodological foundation for the design of such mechanisms.

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  • 收稿日期:2025-03-10
  • 最后修改日期:2025-10-10
  • 录用日期:2025-11-03
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