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摘要:
The shaft mechanical face seal in a high-speed turbopump of a liquid rocket engine often operates under extremely harsh conditions. For example, a low-temperature and low-viscosity fluid (such as liquid oxygen or liquid hydrogen) is used as a lubricant. The performance of the seal rings, especially the friction and wear behavior, directly determines whether the seal functions normal. In this study, the friction and wear behavior of several ring materials are tested using a pin-on-disk tribo-tester, and the wear morphology of the ring is investigated. The friction coefficients (COFs) and mass-wear rates under dry-friction and water-lubricated conditions, which are used to simulate low-viscosity conditions, are obtained. The results show that at a pressure–velocity (PV) value of 2.4 MPa·(m/s), the COF between the copper graphite (stator) and copper–chrome alloy disk (rotor) is low (with a value of 0.18) under the dry-friction conditions, and the 5-min wear mass of the copper graphite is approximately 2 mg. Under the water-lubricated conditions, compared with other materials (such as copper–chrome alloy, S07 steel, alumina ceramic coating, and nickel-based calcium fluoride), the S07 steel with a diamond-like carbon film is preferred for use in a high-speed turbopump under extreme conditions. The results of this study can provide theoretical and experimental guidance in the design of mechanical face seals in liquid rocket engines.
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篇名 Friction and wear behavior of different seal materials under water-lubricated conditions
来源期刊 摩擦(英文版) 学科
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年,卷(期) 2021,(4) 所属期刊栏目 Research Articles
研究方向 页码范围 697-709
页数 13页 分类号
字数 语种 英文
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摩擦(英文)
双月刊
2223-7690
10-1237/TH
北京市海淀区清华大学建筑学院
eng
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