华南理工大学学报(自然科学版) ›› 2013, Vol. 41 ›› Issue (12): 75-80.doi: 10.3969/j.issn.1000-565X.2013.12.013

• 动力与电气工程 • 上一篇    下一篇

二冲程发动机活塞裙部变形和润滑的数值分析

姬芬竹1 杜发荣2† 刘慎微1   

  1. 1.北京航空航天大学 交通科学与工程学院,北京 100191; 2.北京航空航天大学 能源与动力工程学院,北京 100191
  • 收稿日期:2013-04-08 出版日期:2013-12-25 发布日期:2013-11-19
  • 通信作者: 杜发荣(1963-),男,副教授,主要从事活塞发动机研究. E-mail:dfr@buaa.edu.cn
  • 作者简介:姬芬竹(1963-),女,博士,副教授,主要从事活塞发动机研究. E-mail:jfz@buaa.edu.cn
  • 基金资助:

    总装备部预研项目(40109/02010101, 2012076/2001)

Numerical Analysis of Deformation and Lubrication for Piston Skirt of Two- Stroke Engine

Ji Fen- zhu1 Du Fa- rong2 Liu Shen- wei1   

  1. 1.School of Transportation Science and Engineering,Beihang University,Beijing 100191,China;2.School of Energy and Power Engineering,Beihang University,Beijing 100191,China
  • Received:2013-04-08 Online:2013-12-25 Published:2013-11-19
  • Contact: 杜发荣(1963-),男,副教授,主要从事活塞发动机研究. E-mail:dfr@buaa.edu.cn
  • About author:姬芬竹(1963-),女,博士,副教授,主要从事活塞发动机研究. E-mail:jfz@buaa.edu.cn
  • Supported by:

    总装备部预研项目(40109/02010101, 2012076/2001)

摘要: 发动机工作时活塞裙部的变形会直接影响与缸套的配合间隙和润滑状态.文中以某通用航空二冲程活塞发动机为研究对象,建立活塞-活塞销-连杆-气缸套组合体有限元模型,计算并分析了不同负荷作用下活塞裙部的变形,并通过建立二阶运动动力学模型分析了活塞的横向位移,对活塞裙部与气缸套间的润滑油膜厚度和油膜压力进行了模拟计算.结果表明:不同负荷作用下活塞裙部主推力面有不同的变形;热负荷使裙部膨胀变形;机械负荷作用下裙部上端膨胀、下端收缩;热-机负荷耦合作用时的裙部变形复杂,不是两者的简单叠加;发动机工作时裙部两端与气缸套壁面间形成楔形空间,活塞裙部与气缸套之间能够建立油膜润滑.

关键词: 二冲程发动机, 活塞裙部, 变形, 润滑, 数值分析

Abstract:

The deformation of piston skirt directly affects the assembly clearance with cylinder liner and the lubrica-tion state during the engine operation.In this paper,by taking a general aviation two- stroke piston engine as the re-search object,a finite element model describing the piston- piston pin- connecting rod- cylinder liner assembly is con-structed,the deformation of piston skirt under different loads is calculated and discussed,and a second- order dy-namic model is set up to analyze the lateral displacement of the piston.Moreover,the thickness and pressure of thelubricant film between the piston skirt and the cylinder liner are simulated.The results show that (1) the mainthrust plane of the skirt is of a deformation varying with the load; (2) thermal load may result in a skirt expansionand mechanical load may cause an expansion of the skirt upper end as well as a contraction of the lower end of theskirt; (3) under coupled thermal- mechanical load,the deformation of the skirt is not the sum of the deformationsrespectively under thermal and mechanical loads but varies complicatedly; and (4) during the operation of the en-gine,a wedge- shaped space may occur between the ends of the piston skirt and the wall of the cylinder liner,whichmakes the appearance of film lubrication between the piston skirt and the cylinder liner possible.

Key words: two- stroke engine, piston skirt, deformation, lubrication, numerical analysis