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Author:

Wang, Mingkai (Wang, Mingkai.) | Yan, Ke (Yan, Ke.) | Ma, Shuaijun (Ma, Shuaijun.) | Hong, Jun (Hong, Jun.)

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Abstract:

Due to the inconformity of assembly stress and thermal expansion transfiguration in the internal components of shaft systemthe precision angular contact ball bearing could be ap plied into the combined loads consisting of axial load radial load and torque which affected both the dynamic characteristics of bearing and the service performance of precision shaft system. According to the relationship of interaction and relative position between the rolling element and bearing tracka fivedegreeoffreedom quasistatic model considering the effects of centrifugal forcegyroscopic torque and other nonlinear factors was establishedand the calculation model of bearing stiffness was improved by the principle of stepbystep search method. The evolution ary regularity of dynamic characteristics for precision angular contact ball bearings was investigat ed in combined loads. The results indicated that the axial load could decrease the difference be tween ballinner raceway contact angle and ballouter raceway contact angle and suppress the stiffness softening caused by the increase of speed. When the torque and radial force were applied separately the fluctuation range of contact angle and contact force increased and the bearing stiffness along the direction of loads also increasedwhile the stiffness decreased perpendicularly to this direction. In the condition of combined loadsthe torque would restrain the fluctuation of load distribution due to the radial loadand improve the loading capacity and service life of preci sion ball bearing. © 2022 BUAA Press. All rights reserved.

Keyword:

Axial loads Ball bearings Contact angle Roller bearings Stiffness Thermal expansion

Author Community:

  • [ 1 ] [Wang, Mingkai]Key Laboratory of Education Ministry for Modern Design and RotorBearing System, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 2 ] [Yan, Ke]Key Laboratory of Education Ministry for Modern Design and RotorBearing System, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 3 ] [Ma, Shuaijun]Key Laboratory of Education Ministry for Modern Design and RotorBearing System, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 4 ] [Hong, Jun]Key Laboratory of Education Ministry for Modern Design and RotorBearing System, Xi'an Jiaotong University, Xi'an; 710049, China

Reprint Author's Address:

  • K. Yan;;Key Laboratory of Education Ministry for Modern Design and Rotor‑Bearing System, Xi'an Jiaotong University, Xi'an, 710049, China;;email: yanke@mail.xjtu.edu.cn;;

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Source :

Journal of Aerospace Power

ISSN: 1000-8055

Year: 2022

Issue: 6

Volume: 37

Page: 1134-1149

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count: 6

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 0

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