• Complex
  • Title
  • Author
  • Keyword
  • Abstract
  • Scholars
Search

Author:

Jing, Xin (Jing, Xin.) | Cao, Hongrui (Cao, Hongrui.) | Chen, Xuefeng (Chen, Xuefeng.) (Scholars:陈雪峰)

Indexed by:

EI Scopus CSCD PKU Download Full text

Abstract:

The relationship between the cage slip ratio and characteristic frequencies was obtained by theoretical deduction. The correctness of the derivation formulas was verified by the rotor experiment bench supported by cylindrical roller bearings. And the variation law of the slip ratio of the cage, the actual characteristic frequencies and the theoretical values deviations with the rotational speed were studied. Results showed that the slip ratio and the deviation tended to increase with the growth of the shaft rotating speed. The research conclusion has the guiding significance for the fault diagnosis of the aeroengine main-bearings. © 2019, Editorial Department of Journal of Aerospace Power. All right reserved.

Keyword:

Aircraft engines Cylindrical roller bearings Roller bearings

Author Community:

  • [ 1 ] [Jing, Xin]Aeroengine Research Institute, School of Mechanical Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 2 ] [Cao, Hongrui]Aeroengine Research Institute, School of Mechanical Engineering, Xi'an Jiaotong University, Xi'an; 710049, China; State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 3 ] [Chen, Xuefeng]Aeroengine Research Institute, School of Mechanical Engineering, Xi'an Jiaotong University, Xi'an; 710049, China; State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an; 710049, China

Reprint Author's Address:

  • [Cao, Hongrui]Aeroengine Research Institute, School of Mechanical Engineering, Xi'an Jiaotong University, Xi'an; 710049, China;;[Cao, Hongrui]State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an; 710049, China;;

Show more details

Related Keywords:

Source :

Hangkong Dongli Xuebao/Journal of Aerospace Power

ISSN: 1000-8055

Year: 2019

Issue: 5

Volume: 34

Page: 1145-1152

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 9

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 1

FAQ| About| Online/Total:1168/203915641
Address:XI'AN JIAOTONG UNIVERSITY LIBRARY(No.28, Xianning West Road, Xi'an, Shaanxi Post Code:710049) Contact Us:029-82667865
Copyright:XI'AN JIAOTONG UNIVERSITY LIBRARY Technical Support:Beijing Aegean Software Co., Ltd.