Performance of a novel foil bearing with top foil thickness variation in axial direction
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(1. School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China; 2. Nanjing Engineering Institute of Aircraft Systems, Jincheng Aviation Industry Corporation of China, Nanjing 211102, China)

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V229;TH133.37

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    Abstract:

    To improve the foil bearing performance, a novel foil journal bearing with top foil thickness variation in axial direction was proposed. A wide groove extending in circumferential direction, within micron magnitude, was manufactured in the mid-plane zone of top foil. To consider the top foil thickness variation, the 2D thick plate finite element model was employed to simulate the top foil deformation. Based on Newton-Raphson iterative method and finite difference method, the coupled pressure equation and foil deflection equation were solved, and the gas pressure distribution and load capacity of the novel foil bearing were obtained. The dynamic characteristics were solved using perturbation method and the influence of the wide groove depth on bearing performance was investigated theoretically. The results indicate that the novel foil bearing with top foil thickness variation axially can decrease the gas edge leakage and improve hydrodynamic pressure effectively, so the load capacity and dynamic characteristics are improved. Moreover, with the increment of the wide groove depth on top foil, the load capacity and direct stiffness are enhanced further. For the foil journal bearing with a wide groove depth of 8 μm, the load capacity and direct stiffness increase by about 11.8% and 12.1% respectively, compared with the traditional foil journal bearing.

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History
  • Received:March 06,2017
  • Revised:
  • Adopted:
  • Online: January 11,2018
  • Published:
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