Fatigue Measurement for Remaining Life

Abstract

The objective of this work was to follow track pin surface residual stress as a function of fatigue test cycles. Twenty pins were selected from a group of 250 new T-142 track pins for this test. They were selected on the basis of being representative of pins having median values of surface residual stress as received from the shot peening operation in manufacturing. Residual stress measurements were made in both the longitudinal direction and hoop/transverse direction at three spots on each pin. The spots were at areas most likely to develop cracking and eventual failure. The equipment used for residual stress measurement was automated X-ray diffraction equipment. Surface residual stress was found to remain virtually unchanged throughout the entire two million cycles of fatigue testing. Pins failing prior to the two million cycle test limit displayed no residual stress indication that failure was eminent.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1984
Accession Number
ADA149635

Entities

People

  • S. B. Catalano

Organizations

  • United States Army Tank Automotive Research, Development and Engineering Center

Tags

DTIC Thesaurus Topics

  • Diffraction
  • Dynamic Loads
  • Engineering
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Information Exchange
  • Manufacturing
  • Materials
  • Materials Testing
  • Measurement
  • Mechanics
  • Residual Stress
  • Residuals
  • Shot Peening
  • Stresses
  • X Rays
  • X-Ray Diffraction

Readers

  • Aerospace Test and Evaluation
  • Structural Health Monitoring of Composite Structures.