弹用涡喷发动机润滑油系统动密封结构研究

推进技术 ›› 2002, Vol. 23 ›› Issue (1): 57-59.

弹用涡喷发动机润滑油系统动密封结构研究

刘艳梅,李东,刘振德,王黎钦,古乐,齐毓霖

航天科工集团公司31所;北京100074;航天科工集团公司31所;北京100074;航天科工集团公司31所;北京100074;航天科工集团公司31所;北京100074;哈尔滨工业大学机械工程系 ;黑龙江哈尔滨150001;哈尔滨工业大学机械工程系 ;黑龙江哈尔滨150001

发布日期:2021-08-15

Structure of dynamic seal used in the lubricating system of a missile turbojet engine

The 31st Research Inst.,Beijing 100074,China;The 31st Research Inst.,Beijing 100074,China;The 31st Research Inst.,Beijing 100074,China;The 31st Research Inst.,Beijing 100074,China;Dept.of Mechanical Engineering, Harbin Inst. of Technology, Harbin 150001,China;Dept.of Mechanical Engineering, Harbin Inst. of Technology, Harbin 150001,China

Published:2021-08-15

摘要/Abstract

摘要： 论述了某弹用涡喷发动机动密封结构工作原理及泄漏失效形式 ,对润滑系统的动密封结构进行了密封元件的研制 ,配合零件间隙的设计和台架模拟的试验研究 ,掌握了该发动机动密封的磨损机理。台架试验结果证明了其动密封结构设计的合理性

关键词: 涡轮喷气发动机;润滑系统;动密封;金属密封件

Abstract: The working mechanism of dynamic seal and the leakage failure of sealing system were discussed according to the structure of a missile turbojet engine. The development of the sealing units, fitting tolerance design and simulation bench tests of a special dynamic sealing system used in a missile turbojet engine were completed, and its wear mechanism was clarified. Test results showed that the structure design is correct.

Key words: Turbojet engine;Lubrication system;Dynamic sealing;Metallic seal

刘艳梅,李东,刘振德,王黎钦,古乐,齐毓霖. 弹用涡喷发动机润滑油系统动密封结构研究[J]. 推进技术, 2002, 23(1): 57-59.