Hostname: page-component-cd9895bd7-mkpzs Total loading time: 0 Render date: 2024-12-25T05:11:14.404Z Has data issue: false hasContentIssue false

Design and simulation of an aircraft brake using a digital computer

Published online by Cambridge University Press:  04 July 2016

J. S. Claridge BSc*
Affiliation:
Dunlop Ltd

Extract

In order to test a proposed design of aircraft brake, it is obviously necessary to build a prototype, lay down a testing schedule in accordance with airworthiness requirements, and then test the brake, using for example a flywheel type test machine.

The time scale involved in this exercise is quite considerable. Once the brake has been designed it has to be drawn, stressed and the paper work required to make the prototype raised. What is not quite so obvious is that in most cases of brake test the final stage or reject take-off test leads to destruction of the heat sink. Thus if the test is not satisfactory or the results do not comply with the requirements and a retest is required, then a new prototype will also be required. In the case of a large multiplate disc brake the cost of such an exercise would be considerable.

It is hoped that the introduction of a “simulator” program run on a digital machine will enable a good deal of both time and money to be saved in the evolution of a satisfactory design.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1973 

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.)