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Developments in Aircraft Fasteners: A Review of the Properties of Titanium Bolts, Higher‐Strength Steel Bolts and Lightweight Nuts Produced by T. J. Brooks (Leicester) Ltd.

R.T. Allsop B.Sc, Ph.D. (Products Manager, G.K.N. Screws and Fasteners Ltd., P.O. Box No. 24, Heath Street, Birmingham.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1964

90

Abstract

IN recent years the rapid development of aircraft, both military and civil, has generated a demand for improved fasteners to replace the standard range of steel bolts and nuts which have been in use for many years. This demand may be conveniently divided into three sections as follows:

Citation

Allsop, R.T. (1964), "Developments in Aircraft Fasteners: A Review of the Properties of Titanium Bolts, Higher‐Strength Steel Bolts and Lightweight Nuts Produced by T. J. Brooks (Leicester) Ltd.", Aircraft Engineering and Aerospace Technology, Vol. 36 No. 3, pp. 69-72. https://doi.org/10.1108/eb033848

Publisher

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MCB UP Ltd

Copyright © 1964, MCB UP Limited

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