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[1]赵伟刚,张鹏鹏,任姗姗,等.液体火箭发动机涡轮泵机械密封磨损机理研究[J].火箭推进,2017,43(03):10-16.
　ZHAO Weigang,ZHANG Pengpeng,REN Shanshan,et al.Research on wear mechanism of mechanical seal for turbopump in liquid rocket engine[J].Journal of Rocket Propulsion,2017,43(03):10-16.
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液体火箭发动机涡轮泵机械密封磨损机理研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 43 期数: 2017年03期 页码: 10-16 栏目: 研究与设计 出版日期: 2017-08-01
Title:
Research on wear mechanism of mechanical seal for turbopump in liquid rocket engine
作者:
赵伟刚1; 张鹏鹏2; 任姗姗2; 董光能2
1. 西北工业大学 航天学院，陕西 西安 710072； 2. 西安交通大学 现代设计及转子轴承系统教育部重点实验室，陕西 西安 710049
Author(s):
ZHAO Weigang1;  ZHANG Pengpeng2;  REN Shanshan2;  DONG Guangneng2
1. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China; 2. MOE Key Laboratory for Modern Design and Rotor-bearing System, Xi’an Jiaotong University, Xi’an 710049, China
关键词:
表面形貌; 仿真分析; 机械密封; 磨损机理
Keywords:
surface topography;  simulation analysis;  mechanical seal;  wear mechanism
分类号:
V433-34
文献标志码:
A
摘要:
对比分析了机械密封静环端面原始表面和磨损表面形貌，得到了磨损形式和内外径磨损差异；仿真分析了密封端面接触应力及温度场，分析了转速、介质压力等条件对端面接触应力和温度场的影响；探明了端面接触应力和温度变化对磨损性能的影响，阐述了机械密封的磨损机理。
Abstract:
The original surface morphology and the worn surface morphology of static ring end-face of mechanical seal was analyzed by metallographic microscope. The wear form and the differences between inner diameter and outer diameter were obtained. The contact stress and temperature field distribution on the seal end-face are analyzed by means of simulation. The influences of rotating speed, medium pressure and other conditions on end-face contact stress and temperature field are also analyzed by means of ANSYS software platform. The effect of end-face contact stress and temperature variation on the properties of wear was verified. The wear mechanism of mechanical seal was expounded.

参考文献/References:

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备注/Memo

收稿日期：2016-10-25；修回日期：2017-01-06 基金项目：民用航天产品高可靠长寿命专项（〔2014〕618号） 作者简介：赵伟刚（1977—），男，高级工程师，研究领域为机械密封

更新日期/Last Update: 1900-01-01