DocumentCode
982084
Title
Boeing 777 high lift control system
Author
Rea, Jon
Author_Institution
Boeing Commercial Airplane Group, Seattle, WA, USA
Volume
8
Issue
8
fYear
1993
Firstpage
15
Lastpage
21
Abstract
The Boeing 777 high lift control systems (HLCS), a state-of-the-art microprocessor-based system that provides fly-by-wire control, protection, and built-in-test and maintenance access functions for the leading edge slats and trailing edge flaps drive and actuation systems, is discussed. This system is designed to take advantage of technologically proven concepts as well as judicious application of new concepts in response to market demands, airline customer input, and a thorough review of lessons learned from previous aircraft programs. The purpose of the HLCS, the wing high lift devices it controls, the HLCS components, its three modes of operation, automatic functions, and system failure protections are described. The use of the EASY5 engineering analysis program developed by the Boeing Company to model dynamic systems in both the time and frequency domains for modeling mechanical and hydraulic portions of the high lift system is discussed.<>
Keywords
aircraft control; aircraft instrumentation; computerised control; microcomputer applications; protection; Boeing 777 high lift control systems; EASY5 engineering analysis program; actuation; built-in-test; dynamic systems; fly-by-wire control; hydraulic system; leading edge slats; maintenance; mechanical system; microprocessor; system failure protections; trailing edge flaps drive; wing high lift devices; Aerospace electronics; Automatic control; Communication switching; Communication system control; Computer displays; Control systems; Electric variables control; Radio control; Switches; Valves;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/62.248331
Filename
248331
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