首页 | 本学科首页   官方微博 | 高级检索  
     

钛铝涡轮轴与K418合金轴套过盈配合内应力分析
引用本文:曹睿,李雷,张继,何洪,陈剑虹. 钛铝涡轮轴与K418合金轴套过盈配合内应力分析[J]. 理化检验(物理分册), 2010, 0(9): 552-556
作者姓名:曹睿  李雷  张继  何洪  陈剑虹
作者单位:[1]兰州理工大学甘肃省有色金属新材料省部共建国家重点实验室,兰州730050 [2]西安赛特金属材料开发有限公司,西安710021 [3]钢铁研究总院,北京100081 [4]中国北方发动机研究所,大同037036
基金项目:柴油机高增压技术国防科技重点实验室基金项目(9140C3309020803);国家自然科学基金顶目(50905081)
摘    要:通过有限元ABAQUS软件对钛铝涡轮轴与K418合金轴套的过盈配合进行了详细研究,分别从过盈量、连接件几何结构和装配长度等因素入手,分析了压装过程中应力的变化情况,指出应力最大的位置,从理论上提出降低应力和提高寿命的措施。比较钛铝涡轮轴与K418合金轴套不同过盈量下及不同接触长度下过盈配合装配的应力分布结果,表明过盈量是影响装配应力的主要因素,得出较合理的过盈量应在0.15 mm左右,装配接触长度对装配应力也有一定影响。通过不同过渡圆角的模拟计算发现过渡圆角的大小对应力的影响较大,与压装过程中出现的应力峰值有直接的关系。所以在设计时可以采取在合适的范围内增大过渡圆角或添加去应力槽的方式减小应力集中现象,从而降低装配过程中出现的应力峰值,减少对涡轮轴材料的损伤。

关 键 词:钛铝涡轮轴  K418合金轴套  过盈配合  有限元计算  应力分布

Internal Stress Analysis of Interference Fittings of TiAl Turbine Shaft and K418 Alloy Sleeve
CAO Rui,LI Lei,ZHANG Ji,HE Hong,CHEN Jian-hong. Internal Stress Analysis of Interference Fittings of TiAl Turbine Shaft and K418 Alloy Sleeve[J]. Physical Testing and Chemical Analysis Part A:Physical Testing, 2010, 0(9): 552-556
Authors:CAO Rui  LI Lei  ZHANG Ji  HE Hong  CHEN Jian-hong
Affiliation:1. State Key Laboratory of Gansu Advanced Non-ferrous Metal Materials, Lanzhou University of Technology, Lanzhou 730050,China; 2. Xi'an Dorset Metal Materials Development Co. Ltd. , Xi'an 710021, China; 3. Central Iron and Steel Research Institute, Beijing 100081, China; 4. China North Engine Research Institute, Datong 037036, China)
Abstract:Interference fittings of TiAl turbine shaft and K418 alloy sleeve were studied by the software of finite element method ABAQUS. The variation of stresses in assembling process were simulated and calculated by different fit tolerances, geometry and contact lengths. The danger situation of the shaft and sleeve was found by analyzing the stress distribution, and the measures were put forward to decrease contact stress and improve performance life. By comparison of stress distribution results of the different fit tolerances and different contact length, it was shown that fit tolerance had a main effect on the contact stress, and fit tolerance of 0. 15 mm was the optimal choose. And the contact lengths had some effect on the contact stress too. Simulated results at different transitional arc radius showed that it affected contact stress heavily, and it was concerned maximum contaet stress in the assembling process. So these effects were considered in design process to reduce the material damage, stress concentration and maximum contact stress were reduced by increasing transitional arc radius or add stress relieving slot.
Keywords:TiAl turbine shaft  K418 alloy sleeve  interference fitting  finite element method calculation  stress distribution
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号