Abstract. There are considerably rigorous requirements for accuracy
and stability of the mechanism to accomplish large-scale and complex surface
machining tasks in the aerospace field. In order to improve the stiffness
performance of the parallel mechanism, this paper proposes a novel three
degrees of freedom (DOF) redundantly actuated 2RPU-2SPR (where R, P, U and
S stand for revolute, prismatic, universal and spherical joints,
respectively) parallel mechanism. Firstly, the kinematics position inverse
solution is derived and a dimensionless generalized Jacobian matrix is
established through the driving Jacobian matrix and constraint Jacobian
matrix. Secondly, the stiffness model of the parallel mechanism is deduced and
the accuracy of the stiffness model is verified through finite-element analysis. Using eigenscrew decomposition to illustrate the physical interpretation of the
stiffness matrix, the stiffness matrix is equivalent to six simple screw
springs. Finally, the simulation experiment results demonstrate that
redundantly actuated parallel mechanism has better stiffness performance
compared to the traditional 2RPU-SPR parallel mechanism.