冯军, 王禺林, 柳明明, 等. 应用于舱外空间环境的对接锁紧机构设计[J]. 真空与低温, 2020, 26(6): 503-507. DOI: 10.3969/j.issn.1006-7086.2020.06.013
引用本文: 冯军, 王禺林, 柳明明, 等. 应用于舱外空间环境的对接锁紧机构设计[J]. 真空与低温, 2020, 26(6): 503-507. DOI: 10.3969/j.issn.1006-7086.2020.06.013
FENG Jun, WANG Yulin, LIU Mingming, et al. Design of Docking and Locking Mechanism for Extravehicular Vacuum Environment[J]. VACUUM AND CRYOGENICS, 2020, 26(6): 503-507. DOI: 10.3969/j.issn.1006-7086.2020.06.013
Citation: FENG Jun, WANG Yulin, LIU Mingming, et al. Design of Docking and Locking Mechanism for Extravehicular Vacuum Environment[J]. VACUUM AND CRYOGENICS, 2020, 26(6): 503-507. DOI: 10.3969/j.issn.1006-7086.2020.06.013

应用于舱外空间环境的对接锁紧机构设计

Design of Docking and Locking Mechanism for Extravehicular Vacuum Environment

  • 摘要: 根据空间站实验舱外暴露载荷的需求以及现有机械臂的抓举能力,开展了暴露载荷与空间站资源传输设备——对接锁紧机构的设计。主要进行了机构总体设计和误差分析,针对舱外真空、高低温交变、辐照等环境进行了抗环境效应设计,针对发射时的力学冲击进行了仿真计算。系列验证试验表明,设计能够满足使用要求。

     

    Abstract: According to the demand of the space station experiment cabin extravehicular expose payload and the mechanical arm snatch ability,we design the docking and locking mechanism which transfers the resource of space station to the expose payload.To suit the vacuum,high and low temperature alternating,irradiative environment we have finished special designing.To suit the dynamic environment during the launch phase we have finished dynamics simulating and calculating,besides that a series of experiments approves that the designing satisfies the demand of using.

     

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