空间楔形自锁式重复锁紧机构

A Repeated Locking Device for Space Vehicles Based on Wedge Self-locking Principle

  • 摘要: 针对宇宙真空环境下, 舱外机械臂或航天员操作下的在轨可更换单元重复锁紧困难的问题,研究了一种以电动为主、航天员手动操作为辅的空间楔形自锁式重复锁紧机构。设计了锁紧执行机构和驱动机构,确定了锁紧驱动力、滑移面材料等关键参数。结果表明,10 kg的原型机承载能力达到350 kg,能够适应舱外机械臂或EVA操作,受载条件下自锁可靠、定位精度良好,−45~60 ℃的真空环境下运动可靠,锁紧和解锁功能正常。

     

    Abstract: In the vacuum, high and low temperatures, space radiation and other cosmic environments of the universe, aiming at the problem of repeated locking orbital replacement unit based on manipulator operating, planetary extravehicular activity (EVA) and the operation of the manipulator cooperating with the operation of the astronaut cabin, a repeated locking device based on wedge self-locking principle which could be mainly electric or manual operated was put forward in this paper. Extravehicular activity (EVA) is one of the most dangerous activities of human space exploration. In order to ensure the safety of astronauts and the success of missions, it is imperative to identify and mitigate the inherent risks and challenges associated with EVAs. Space robots have high mission flexibility, working ability and operational accuracy, and have the ability to replace astronauts to complete dangerous tasks. Robot operation replaces astronauts' out-of-cabin operations, which will greatly reduce the danger of astronauts, and save the airlock opening life and gas resources of the aircraft. The lock actuator and lock driver of the repeated locking device for space vehicles based on wedge self-locking principle were meticulously, comprehensively and cleverly designed. The key technologies of lock driving force and slip surface material were determined. The results of the load capacity test, life test, manipulator operation matching test and thermal vacuum environment test showed that the prototype sets with deadweight of 10 kg could bear the weight of 350 kg and could adapt to manipulator operating and EVA and had the advantages of self-locking and positioning accuracy under load. This device could adapt to the vacuum temperature of −45~60 ℃ and had the advantages of reliably locking and unlocking movement. In the subsequent space docking mechanism or locking mechanism design process, it can be given priority as an alternative configuration. It can improve the level of China's related space repeatable locking technology, and lay a solid foundation for China's space industry.

     

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