Flat Bus Fault Sensors.

Abstract

This report documents the development of an electric power distribution fault sensing technique for use on a 270 Vdc, two wire, flat bus, ungrounded aircraft power distribution system for operation in composite aircraft structures. The effort, performed by the Strategic Systems Division of Rockwell International, included the development, fabrication and delivery of six fault sensor breadboards. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1979
Accession Number
ADA077060

Entities

People

  • Carl O. Linder

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Aircrafts
  • Composite Aircraft
  • Composite Materials
  • Composite Structures
  • Detection
  • Detectors
  • Electric Power
  • Electronics
  • Fabrication
  • Generators
  • Hall Effect
  • Materials
  • Materials Processing
  • Power Distribution
  • Resistance
  • Schematic Diagrams
  • Short Takeoff Aircraft

Readers

  • Electrical Engineering
  • Software Engineering