Title :
Design of Boeing 777 electric system
Author :
Andrade, Luiz ; Tenning, Carl
Author_Institution :
Sundstrand Aerosp. Electr. Power Syst., Rockford, IL, USA
fDate :
7/1/1992 12:00:00 AM
Abstract :
The electric power system for the Boeing 777 is comprised of two independent electrical systems, the main and the backup. The main electric system includes two engine-driven integrated drive generators, a generator driven by the auxiliary power unit, three generator control units, and a bus power control unit. The backup electric system includes two engine-drive generators and one integrated converter/control unit to provide the redundancy of electrical sources equivalent to a three-engine airplane. Automation of the system is achieved by the use of state-of-the-art, microprocessor-based control units that perform system control, protection, and built-in-test functions. Each control unit has redundant two-way communication through an ARINC 629 communication bus that requires significantly fewer discrete wires than similar systems, allowing considerable reduction of the interface circuits and reduction in weight.<>
Keywords :
aircraft control; built-in self test; power supplies to apparatus; power system computer control; protection; redundancy; ARINC 629 communication bus; Boeing 777; auxiliary power; backup; built-in-test; bus power control; engine-driven integrated drive generators; integrated converter/control; main electric system; protection; redundancy; Airplanes; Automatic control; Automatic generation control; Automation; Communication system control; Control systems; Power control; Power generation; Power system protection; Standby generators;
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE