Title :
REACTS: reliable electrical actuation systems
Author :
Dixon, R. ; Gifford, N. ; Sewel, C. ; Spalton, M.C.
Author_Institution :
ABB ALSTOM POWER Technol. Centre, Leicester, UK
fDate :
6/21/1905 12:00:00 AM
Abstract :
For future generation aircraft a number of initiatives are in progress worldwide examining the concept of the More/All Electric Aircraft, including the development of the More/All Electric Engine. The Reliable Electrical Actuation Systems (REACTS) programme, which is being part funded by the UK Department of Trade and Industry (DTI), is a multi-company research initiative with the aim of demonstrating the potential for replacing current hydraulic/pneumatic/fueldraulic engine actuation systems on civil aircraft with electromechanical equivalents. The actuators which control the engine variable inlet guide vanes (VIGVs) and the variable stator vanes (VSVs) have been identified for investigation and a concept demonstrator actuation system is being developed. This paper provides the background and requirement for the REACTS programme, and discusses the three major sections of work, namely: control and drive electronics, electromechanical design, and system modelling and fault detection, isolation and accommodation (FDIA)
Keywords :
electric actuators; All Electric Aircraft; All Electric Engine; More Electric Aircraft; More Electric Engine; REACTS; Reliable Electrical Actuation Systems programme; UK Department of Trade and Industry; civil aircraft; drive electronics; electromechanical design; electromechanical equivalents; engine variable inlet guide vanes control; fault accommodation; fault detection; fault isolation; multi-company research initiative; reliable electrical actuation systems; variable stator vanes control;
Conference_Titel :
Electrical Machines and Systems for the More Electric Aircraft (Ref. No. 1999/180), IEE Colloquium on
Conference_Location :
London
DOI :
10.1049/ic:19990834