大行程柔性微定位平台的伴生转动分析  

Parasitic rotation of large stroke compliant micro-positioning platform

作　　者：孟刚 黄河 吴伟官 居勇健 曹毅 MENG Gang;HUANG He;WU Weiguan;JU Yongjian;CAO Yi(School of Mechanical Engineering,Jiangnan University,Wuxi 214122,China;Jiangsu Key Laboratory of Advanced Food Manufacturing Equipment and Technology,Wuxi 214122,China)

机构地区：[1]江南大学机械工程学院,无锡214122 [2]江苏省食品先进制造装备技术重点实验室,无锡214122

出　　处：《北京航空航天大学学报》2023年第3期665-673,共9页Journal of Beijing University of Aeronautics and Astronautics

基　　金：江苏省“六大人才高峰”计划(ZBZZ-012);高等学校学科创新引智计划(B18027);江苏省研究生创新计划(KYCX20-1925)。

摘　　要：大行程柔性微定位平台在运动过程中不可避免地产生伴生转动现象,并对其定位精度造成消极影响。为降低伴生转动对平台定位精度的影响,提出一种基于柔性杆的三移一转(3-PPPR)型大行程柔性微定位平台,基于线弹性梁理论模型并考虑柔性杆轴向形变,对两移一转(PPR)柔性运动副伴生转角进行了理论建模,并基于此完成了对所提平台在单轴、双轴及三轴驱动时产生伴生转角的理论分析;再采用有限元分析对理论模型进行验证。最后探究了柔性杆尺寸参数与平台伴生转角之间的灵敏度关系,为所提平台性能提升奠定了基础,并据此提出了改善所提平台运动性能的优化方案。结果表明:3种驱动条件下平台伴生转角理论值与仿真值最大相对误差为2.46%。Parasitic rotation is inevitable during the movement of large stroke compliant micro-positioning platforms,causing a negative impact on their positioning precision.To reduce this effect,a 3-PPPR compliant micropositioning platform with large stroke is proposed based on compliant beams.Then,based on linear elastic beam theory,the theoretical parasitic rotational angle of the PPR compliant kinematic joint is modeled considering the axial deformations of the beams.The parasitic rotational angles of the platform are also analyzed theoretically in uniaxial,biaxial and triaxial cases.Furthermore,the theoretical models are verified by finite element analysis.Finally,the sensitivity between the dimension parameters of the compliant beams and the parasitic rotational angle of the platform is analyzed,laying a foundation for the improvement of the platform.On this basis,the optimization schemes are proposed to improve the motion performance of the platform.results show that the maximum relative errors of the theoretical and simulated values of the parasitic rotational angle is 2.46%in three driven cases.

关 键 词：柔性微定位平台 伴生转动 多轴驱动 有限元仿真 灵敏度分析 

分 类 号：V414.5[航空宇航科学与技术—航空宇航推进理论与工程] TH122[机械工程—机械设计及理论]