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STUDY OF BONDED SOLID FILM LUBRICANTS FOR SPACE STATION LONG TERM LUBRICATION

机译:空间站长期润滑用键合固体薄膜润滑剂的研究

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Bonded solid film lubricants have been used for numerous satellite mechanical components. But future Chinese Space Station Mission put increasing demands on the lubrication requirements for trouble-free service, such as long-life, high load-carrying and atomic oxygen resistance. The objective of this paper is to discuss the future technical requirements and evaluted four kinds of bonded solid film lubricants for high-cycle space station applicants. Three of the lubricants were bonded molybdenum disulfide based solid film lubricants for vacuum, the other one was bonded polytetrafluoroethylene based solid film lubricant for the cosmonauts living environment. The routine technical data including curing temperature, workable temperature range, outgassing properties, load-carrying capacity and adhesion of polyamideimidc bonded, sodium silicate bonded and a duplex bonded molybdenum disulfide based solid film lubricants were compared. The wear lifetime of the three kinds of lubricants were studied by a ball-on-disc tribometer in vacuum at 920 MPa contact stress. And the effects of the atomic oxygen on the lubricants were also discussed, the accumulative total dose of the atomic oxygen which corresponds to 15 years in low earth orbit is 7.83E+26 atom/m2. The total dose of ionizing radiation in space for 15 years were equivalent to 9E+C rad(Si) Co60 gamma exposure in air, but the effect of the radiation on the lubricants must be tested at the close of 2E+7 rad(Si) rigorously. The duplex bonded molybdenum disulfide based solid film lubricants revealed advantages among the three kinds of film lubricants. On the other hand, the hygrothermal effects on the polyamideimide bonded polytetrafluoroethylene based solid film lubricants which would be used in the cosmonauts living environment were also considered. The film lubricants were exposed to a highly aggressive humidity durability test; test conditions were 80 degree centigrade and 95% relative humidity for about 2000 hours. All these test results will be the guide of designing-long-life lubrication systems and chooseing appropriate bonded solid film lubricants for the space station components.
机译:粘结的固体膜润滑剂已用于许多人造卫星机械部件。但是,未来的中国空间站飞行任务对无故障服务的润滑要求越来越高,例如长寿命,高负载和抗原子氧性。本文的目的是讨论未来的技术要求,并为高循环空间站的申请人评估四种粘合固体膜润滑剂。其中三种润滑剂是用于真空的粘合二硫化钼基固体膜润滑剂,另一种是用于宇航员居住环境的粘合聚四氟乙烯基固体膜润滑剂。比较了常规技术数据,包括固化温度,工作温度范围,脱气性,承载能力和聚酰胺亚米德键合,硅酸钠键合和双键键合的二硫化钼固体膜润滑剂的粘合性。通过圆盘球式摩擦计在920 MPa的接触应力下对三种润滑剂的磨损寿命进行了研究。并讨论了原子氧对润滑剂的影响,相当于低地球轨道15年的原子氧累积总剂量为7.83E + 26atoms / m2。太空中15年的电离辐射总剂量等于空气中9E + C rad(Si)Co60γ辐射,但是必须在2E + 7 rad(Si)接近时测试辐射对润滑剂的影响严格地。双键结合的二硫化钼基固体薄膜润滑剂在三种薄膜润滑剂中显示出了优势。另一方面,还考虑了在宇航员居住环境中使用的聚酰胺酰亚胺键合的聚四氟乙烯基固体膜润滑剂的湿热效应。薄膜润滑剂经受了高度侵蚀性的湿气耐久性测试;测试条件为80摄氏度和95%相对湿度,持续约2000小时。所有这些测试结果将为设计长寿命润滑系统以及为空间站组件选择合适的粘结固体膜润滑剂提供指导。

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