Experience of One UK Electronic Equipment Supplier With Bite on Engine/Flight Control Systems Over the Past Ten Years — Part 2

Raymond de Gaye (Engineering Manager, Dowty Electronics (Controls Division))

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 October 1986

Abstract

The ECU safety system is such that all internal and external fault monitoring circuit outputs are consolidated and passed through a short time‐constant filter to eliminate transient effects. Once this signal appears a 500mS time‐out is started. At the end of this period a lane changeover is initiated together with a cockpit fault warning. If the fault condition is removed during the time‐out period, it is reset.

Citation

de Gaye, R. (1986), "Experience of One UK Electronic Equipment Supplier With Bite on Engine/Flight Control Systems Over the Past Ten Years — Part 2", Aircraft Engineering and Aerospace Technology, Vol. 58 No. 10, pp. 10-14. https://doi.org/10.1108/eb036345

Download as .RIS

Publisher

:

MCB UP Ltd

Copyright © 1986, MCB UP Limited

Please note you might not have access to this content

You may be able to access this content by login via Shibboleth, Open Athens or with your Emerald account.
If you would like to contact us about accessing this content, click the button and fill out the form.
To rent this content from Deepdyve, please click the button.