To read this content please select one of the options below:

Criteria for self loosening of fasteners under vibration

GERHARD H. JUNKER (European Research and Engineering Standard Pressed Steel Co, Unbrako, Koblenz)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1972

329

Abstract

A UNIQUE TEST method and apparatus now make it possible to reproduce conditions of vibration that are not only certain to loosen bolted joints but which also closely simulate actual conditions. It can be shown that properly preloaded fasteners loosen as a result of rotation as soon as relative motion occurs between the mating threads and between the bearing surfaces of the fastener and the clamped material.

Citation

JUNKER, G.H. (1972), "Criteria for self loosening of fasteners under vibration", Aircraft Engineering and Aerospace Technology, Vol. 44 No. 10, pp. 14-16. https://doi.org/10.1108/eb034949

Publisher

:

MCB UP Ltd

Copyright © 1972, MCB UP Limited

Related articles