Hostname: page-component-78c5997874-t5tsf Total loading time: 0 Render date: 2024-11-15T04:22:15.274Z Has data issue: false hasContentIssue false

Titanium Structures in Practice

Published online by Cambridge University Press:  04 July 2016

D. Eccles
Affiliation:
Hawker Siddeley Aviation Limited
W. G. Heath
Affiliation:
Hawker Siddeley Aviation Limited

Extract

Developments in the technology have caused a steady decrease in the cost of introducing titanium into aircraft structures. This encouraging state of affairs has resulted in an increased use of titanium alloys, especially in the USA, where the development of supersonic aircraft has provided a prima facie case for their introduction.

In the UK the technology has not developed so rapidly, although both civil and military aircraft have gradually introduced more and more titanium components, principally forgings (see Fig. 1). Some years ago, however, it became apparent that the British aerospace industry could not afford either the time or the money involved in developing the technology for a specific new project. On the other hand, a new project without a substantial percentage of titanium in its structure could well be less efficient than a competitor featuring a large number of titanium components.

Type
Supplementary Papers
Copyright
Copyright © Royal Aeronautical Society 1971 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Paper given at a Symposium on “The Effect of New Materials on Aircraft Design”, on 4th March 1971.