Morphing Wing Based on Trigonal Bipyramidal Tensegrity Structure and Parallel Mechanism

نویسندگان

چکیده

The development of morphing wings is in the pursuit lighter weight, higher stiffness and strength, better flexible ability. A structure that can be used as both bearing mechanism optimal choice for wing. wing composed a tensegrity non-overconstrained parallel was designed. self-balancing trigonal bipyramidal designed based on shape-finding method force-equilibrium equation nodes. 4SPS-RS complete configuration synthesis method. degree freedom inverse solution obtained screw theory, Jacobian matrix established. model relationship between deformation sweep angle, torsion spanwise bending, span obtained. Through modular assembly distributed drive, could perform smooth continuous locally globally. In static state, it has advantages high large capacity. process morphing, motion with four degrees changing sweep, twist,

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ژورنال

عنوان ژورنال: Machines

سال: 2022

ISSN: ['2075-1702']

DOI: https://doi.org/10.3390/machines10100930