Graphite-Fiber Polyimide Composites for Spherical Bearings to 340 deg C (650 deg F)

Abstract

Journal bearings with self-alining spherical elements of graphite-fiber-reinforced - polyimide composites were tested from 24 deg to 340 deg C (75 deg to 650 deg F) at unit loads up 3.5 x 10(exp 7) N/sq m (5000 psi). The journal oscillated in the cylindrical bore of the composite element +/-15 deg at 1 hertz. Outer races and journals were metal hardened to Rockwell C-32 and finished to 10(exp-7)m (4 micro in.) rms. A 45 wt. % graphite-fiber composite gave low friction (0. 08 to 0. 13), low wear, and almost no plastic deformation under any of the test conditions. Composites with 15 and 25 wt.% graphite fiber failed by plastic deformation at 315 deg C (600 deg F) and 3. 5 x 10(exp 7) N/sq m (5000 psi). A composite with 60 wt.% graphite fiber failed by brittle fracture under the same conditions, but had very low friction coefficients (0. 0S to 0. 10) and may be a good bearing material at lighter loads.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1972
Accession Number
ADA375464

Entities

People

  • Harold E. Sliney
  • Robert L. Johnson

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Actuators
  • Airframes
  • Alloys
  • Bearings
  • Composite Materials
  • Control Surfaces
  • Drive Shafts
  • Elements
  • Films
  • Fluoropolymers
  • Friction
  • Graphitic Materials
  • Heat Energy
  • Materials
  • Plastic Deformation
  • Polyimide Resins
  • Thermal Conductivity

Fields of Study

  • Materials science

Readers

  • Powder metallurgy of Titanium alloys.
  • Reinforced Composite Materials
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).