Advanced Battery System for Aircraft.

Abstract

This is the final report on the Advanced Battery System For Aircraft (contract F33615-86-C-2678). This report contains final design and test data on the aircraft battery system and its components developed under this contract by Eagle Picher Industries, Inc. (EPI) (battery development) and ELDEC Corporation (charger/controller development) Figure 1-1 shows the basic battery system. It contains three elements: Battery, Battery Charger, and Controller. Physically the controller and the charger are housed in one Line Replaceable Unit (LRU) . The aircraft interface with the battery system consists of a power interface; three phase input power required is 115Vrms line to neutral at 8A per phase, 400Hz ac bus, and output power is 28Vdc battery bus capable of handling 50A currents. The signal level interface with the aircraft system is in the form of LED drivers for fault and status indication.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1995
Accession Number
ADA336815

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Battery Chargers
  • Circuit Boards
  • Converters
  • Governments
  • High Reliability
  • Lessons Learned
  • Maintenance
  • Manufacturing
  • Materials
  • Power Electronics
  • Reliability
  • Test And Evaluation
  • Test Equipment
  • Transport Aircraft

Readers

  • Battery Technology and Engineering
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Electrical Engineering