Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures

XU Fang-cheng; LIU Zhan-sheng; MA Rui-xian; HUANG Fei-lin

doi:10.13224/j.cnki.jasp.2014.01.028

Chinese

您当前的位置：

首页 >

文章列表页 >

Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures

更新时间：2026-07-07

- Dynamic performance tests of bump-type gas foil journal bearing-rotor system in start-up and shut-down procedures
- Vol. 29, Issue 1, Pages: 216-224(2014)
- 作者机构：
  
  哈尔滨工业大学能源科学与工程学院,哈尔滨,150001
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2014.01.028
  CLC：
- Published：2014
- 稿件说明：
移动端阅览
徐方程, 刘占生, 马瑞贤, 黄飞淋. 波箔型径向气体箔片轴承-转子系统升降速动态特性试验[J]. 航空动力学报, 2014, 29(1): 216-224.

doi: 10.13224/j.cnki.jasp.2014.01.028
徐方程, 刘占生, 马瑞贤, 黄飞淋. 波箔型径向气体箔片轴承-转子系统升降速动态特性试验[J]. 航空动力学报, 2014, 29(1): 216-224. DOI： 10.13224/j.cnki.jasp.2014.01.028.

doi: 10.13224/j.cnki.jasp.2014.01.028 DOI：

摘要

为了研究以波箔型径向气体箔片轴承为支承的轴承-转子系统动力学特性，专门设计了波箔型径向气体箔片轴承试验台，质量为0.458kg的转子在该试验台上实现了超过80000r/min的运转速度.径向轴承为波箔型径向气体箔片轴承，止推轴承为多叶箔片轴承.试验结果表明：波箔型径向气体箔片轴承能够实现转子高速运行，在转子起飞后具有良好的运行稳定性，其轴承支承处振动位移幅值一直维持在20μm之内.由于驱动涡轮受到不平衡气流力的作用，转轴升速时的起飞转速要高于降速时的起飞转速.

Abstract

In order to study the dynamic performance of bearing-rotor system supported by bump-type gas foil journal bearing

a test bed was designed for bump-type gas foil journal bearing. A rotor of 0.458kg including turbine was supported by two bump-type gas foil journal bearings and multi-leaf thrust gas foil bearing

and the speed was more than 80000r/min. The experimental results show that bump-type gas foil journal bearings can offer high-speed operation stability after rotor lift-off

and the vibration displacement amplitude at bearing support is less than 20μm. The rotor lift-off speed in start-up procedure is higher than that in shut-down procedure due to asymmetric drive of turbine.

关键词

Keywords

references

Views

954

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Experimental of foil friction effects on dynamics characteristicof rotor-foil bearing system

Mechanism and effect of “critical follower speed” on dual-rotor system of aero-engines

Performance of air-dynamic lubrication thrust bearing and experiment

Static characteristics analysis of foil thrust bearing considering the rarefield gas effect

Theory and experiment of foil bearing limiting load capacity based on Coulomb friction effect

Related Author

ZHANG Wen

WANG Yu

JIANG Yunfan

LIAO Mingfu

LI Yan

胡斌

李剑雄

王锐

Related Institution

China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation

School of Power and Energy,Northwestern Polytechnical University

Sichuan Gas Turbine Establishment,Aero Engine Corporation of China

北京航空航天大学能源与动力工程学院

中国航天科技集团有限公司北京航天动力研究所

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