PERFORMANCE FACTORS FOR CIRCULAR, HYDROSTATIC, GAS LUBRICATED THRUST BEARINGS. PART III, RING THRUST BEARINGS

A general design procedure for ring type, hydrostatic, gas thrust bearings has been derived. Dimensionless load and flow factors have been calculated for a wide range of bearing parameters using a conformal transformation procedure proposed by Mori and Yabe. These factors are combined with empirical correlations for the bearing entry losses to provide a simple, convenient design procedure. The predicted performances are compared with a number of experimental studies. The results indicate the procedure is adequate for all normal design requirements.

  • Corporate Authors:

    National Research Council of Canada

    National Aeronautical Establishment
    Ottawa, ONo K1A OR6,   Canada 
  • Authors:
    • Dudgeon, E H
    • Maki, M C
  • Publication Date: 1973-3

Subject/Index Terms

Filing Info

  • Accession Number: 00053708
  • Record Type: Publication
  • Source Agency: National Research Council of Canada
  • Report/Paper Numbers: MT-65
  • Files: TRIS
  • Created Date: May 7 1974 12:00AM