Effects of Unfavourable Environmental Conditions on the Service Life of Jet Engine and Helicopter Bearings,

Abstract

Aircraft bearings normally operate at high speeds and have to meet demanding reliability requirements. If conventional guidelines for their design are used, the resultant stresses are low. The stresses are particularly low if compared to those customarily applied in testing rolling fatigue. Testing at such low stress levels was in the past almost entirely relegated to extended performance testing. It was only due to the inexplicably large differences between the calculated fatigue life(unfactored life) and the life actually achieved under normal aircraft-type loading and lubricating conditions that finally led to systematic fatigue life testing.

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1986
Accession Number
ADP005054

Entities

People

  • Georg Schaefer
  • Hans-karl Loroesch

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Engines
  • Fatigue Life
  • Helicopters
  • Jet Engines
  • Performance Tests
  • Reliability
  • Rotary Wing Aircraft
  • Vehicles

Fields of Study

  • Engineering

Readers

  • Systems Analysis and Design
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).