High Speed Cylindrical Roller Bearing Development.

Abstract

High speed experimental tests provided data on six parametric cylindrical roller bearings. Four bearing variables were evaluated and the results were correlated with the analytical model developed under Naval Air Propulsion Center Contract N00140-76-C-0383 with support form the Air Force Aero Propulsion Laboratory MIPRFY14557600623. Roller end clearance was found to have a significant effect on roller end and guide flange wear, whereas the variables roller end circular runout and inner ring guide flange height were both observed to have a moderate effect on water. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1980
Accession Number
ADA095357

Entities

People

  • Edward J. Tobiasz
  • Louis J. Dobek
  • Paul F. Brown

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Body Weight
  • Computer Programs
  • Computers
  • Contracts
  • Experimental Data
  • Failure Mode And Effect Analysis
  • Fatigue Life
  • Governments
  • Manufacturing
  • Measurement
  • Pressure Gages
  • Regression Analysis
  • Statistical Analysis
  • Test And Evaluation
  • Turbines

Readers

  • Aerospace Engineering
  • Metallurgy
  • Structural Dynamics.