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作者机构:China Academy of Space Technology (Xi'an) Xi'an 710100 China School of Mechanical and Electrical Engineering Harbin Institute of Technology Harbin 150001 China Parallel Robot and Mechatronic System Laboratory of Hebei Province Yanshan University Qinhuangdao 066004 China
出 版 物:《IOP Conference Series: Materials Science and Engineering》
年 卷 期:2020年第892卷第1期
摘 要:Aiming at the synchronous motion of tetrahedral deployable unit, the kinematic pair is designed and the coupling motion branch is synthesized based on screw theory. The optimal deployable unit is determined by the application. According to the networking requirements, a networking mechanism composed of multiple units with coupling degree of freedom (DOF) is synthesized. The application of the screw theory in the configuration synthesis of deployable mechanism is realized in this paper. The mechanism is suitable for the deployable mechanism of satellite antenna reflector or other space surface deployable support mechanism, which has broad application prospects.