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RESEARCH PAPERS: Reliability and Fracture Strength Analysis

Reliability of Aircraft Splines With or Without a Wear Induction Period

[+] Author and Article Information
D. Kececioglu

Aerospace and Mechanical Engineering Department, The University of Arizona, Tucson, Ariz.

A. Koharcheck

Bently Nevada Corp., Minden, Nev.

J. Vib., Acoust., Stress, and Reliab 105(2), 163-170 (Apr 01, 1983) (8 pages) doi:10.1115/1.3269080 History: Received May 12, 1982; Online November 23, 2009

Abstract

Mathematical models are developed for the wear-life distributions of aircraft splines which provide equations for predicting their reliability when spline-tooth wear is the failure mode under consideration. The procedure for determining the distributions of wear for specified operating times and of time for specified amounts of spline-tooth wear is presented. Five examples on the use of these distributional data to predict the reliability of aircraft splines and their maintenance schedules are given.

Copyright © 1983 by ASME
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