Accession Number : ADA113633
Title : Advanced Aircraft Electrical System Control Technology Demonstrator. Phase I. Analysis and Preliminary Design.
Descriptive Note : Interim rept. 1 Mar 81-30 Sep 81,
Corporate Author : BOEING MILITARY AIRPLANE CO SEATTLE WA
Personal Author(s) : Boldt,T R ; Dunn,G L ; Hankins,D E ; Leong,P J ; Mehdi,I S
PDF Url : ADA113633
Report Date : Jan 1982
Pagination or Media Count : 134
Abstract : This report summarizes Task 1-Requirements Analysis and Task 2-Conceptual Design and documents the results of Task 3, Phase I, of this two-phase program. Task 3 is the preliminary design of an advanced aircraft electrical system (AAES). The AAES is designed to meet the requirements of a 1990 time frame two-engine tactical aircraft with multi-mission capability. The AAES performs the functions of power generation, distribution and control of power to loads, system protection, and load management. Key characteristics of the AAES are: Integrated avionics and power data bus configuration consisting of Digital Avionics Information System (DAIS) standard elements (MIL-STD-1750 processor, MIL-STD-1553B data bus, controls and displays, and remote terminals (RT)). Intelligent Electrical Load Management Centers (ELMC) capable of controlling power to loads; Built-in-test (BIT) capability to isolate faults to the module level. BIT includes both circuit and data monitoring checks. Solid State Power Controllers (SSPC) to replace circuit breakers and power control switches. SSPCs are turned on/off via computer control. Generator control, protection and status monitoring by a Generator Control Unit (GCU) compatible with DAIS hardware and software. Multimission data information system through programmable system processors, ELMCs and standard DAIS elements. Automatic load management for increased aircraft survivability and probability of mission completion.
Descriptors : *Electric power distribution, *Load control, *Power equipment, *Aircraft equipment, Digital systems, Bus conductors, Power supplies, Systems management, Solid state electronics, Control systems, Electronic switching, Multiplexing
Subject Categories : Aircraft
Electrical and Electronic Equipment
Electric Power Production and Distribution
Distribution Statement : APPROVED FOR PUBLIC RELEASE