主催: 一般社団法人 日本機械学会
会議名: Dynamics and Design Conference 2018
開催日: 2018/08/28 - 2018/08/31
A novel composite structure arm for astronautical development by using CFRP and honeycomb core is already presented. In previous studies, the superiority of the presented arm is theoretically confirmed while experimental results possessed far below stiffness. The reason is estimated to be the failure in adhesion. To avoid this, solid shaping of the arm by using 3D printer is presented. In this study theoretical and experimental evaluation of the presented arm is carried out and their difference are examined.-