The deploy-locking mechanism mounted on the assistant pillar was designed, which can achieve the total deploy of the soft lander before landing.
还设计了安置于辅助支柱的展开锁定机构,可实现软着陆器在着陆前的完全展开。
参考来源 - 月球探测器软着陆缓冲机构方案设计及关键技术研究·2,447,543篇论文数据，部分数据来源于NoteExpress
所述锁定机构在所述轮胎保持位置与所述卡合部卡合。
The lock mechanism is engaged with the engagement portion at the tire holding position.
该锁定机构允许以翻转方式来安装和拆卸上部部分和基座。
This lock mechanism permits the upper part and the base to be mounted and removed in a flipping manner.
快速连接处理与不可分割的锁定机构，确保任何使用微型探头手柄。
Quick-connect handle with integral locking mechanism secures any miniature probe handle in use.
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