Finite element analysis on temperature field of bearing with shaft

WANG Yan-shuang; ZHU Hai-feng; LIU Zhe

Chinese

您当前的位置：

首页 >

文章列表页 >

Finite element analysis on temperature field of bearing with shaft

更新时间：2026-07-07

- Finite element analysis on temperature field of bearing with shaft
- Vol. 27, Issue 5, (2012)
- 作者机构：
  
  1. 河南科技大学机电工程学院,河南,洛阳,471003
  2. 陕西汽车集团汉德车桥有限公司,西安,710201
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2012
- 稿件说明：
移动端阅览
WANG Yan-shuang, ZHU Hai-feng, LIU Zhe. Finite element analysis on temperature field of bearing with shaft[J]. 2012, 27(5).
DOI：

WANG Yan-shuang, ZHU Hai-feng, LIU Zhe. Finite element analysis on temperature field of bearing with shaft[J]. 2012, 27(5). DOI：

摘要

根据轴连轴承组件的结构及特点

建立了有限元模型

实现了对轴连轴承温度场的有限元分析.首先采用拟静力学方法分析出轴承工作时钢球的自转速度

然后计算出轴承在不同的内圈转速、轴向载荷和径向载荷下的功率损失

最后使用ANSYS软件计算出轴承的温度分布.通过算例分析了不同工况对轴连轴承工作温度分布的影响

并进行了试验验证

结果表明:轴向载荷和内圈转速对轴承温度分布影响较大

而径向载荷的变化对轴承温升影响不显著.

Abstract

Finite element model based on the structure of bearing with shaft was set up.Its temperature field was analyzed by finite element method.First

angular speed of balls was analyzed through quasi-static method.Then power loss was gotten at various inner ring velocities

axial loads and radial loads.Finally

temperature distribution was calculated by ANSYS.Effects on temperature field were analyzed at different operating conditions by examples.The results validated by experiments show that axial load and inner ring velocity can affect temperature distribution strongly

but the effect of radial load is not significant.

关键词

Keywords

references

Views

520

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical Simulation of Nacelle Flow and Temperature Field

Infrared radiation signature of three bearing swivel nozzle

Analysis of thermal characteristics of oil⁃cooled aviation wet friction clutch

Thermal characteristics for bearing combined EHL theory with CFD method

Numerical analysis on residual stress of foreign object damage on the leading edge of titanium alloy blade

Related Author

WANG Fang

YU Jian-zu

XIE Yong-qi

Jie SHI

Li ZHOU

Jingwei SHI

Zhanxue WANG

Heyun BAO

Related Institution

Institute of Aeronautical Science and Engineering,Beijing University of Aeronautics and Astronautics

School of Power and Energy，Northwestern Polytechnical University

National Key Laboratory of Science and Technology on Helicopter Transmission，Hunan Aviation Powerplant Research Institute，Aero Engine Corporation of China

National Key Laboratory of Science and Technology on Helicopter Transmission， Nanjing University of Aeronautics and Astronautics

大连民族大学智能感知与先进控制国家民委重点实验室

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰