Accession Number:

ADA336815

Title:

Advanced Battery System for Aircraft.

Descriptive Note:

Final rept. 1 Nov 86-1 Jun 95.

Corporate Author:

EAGLE-PICHER INDUSTRIES INC COLORADO SPRINGS CO ELECTRONICS DIV

Personal Author(s):

Report Date:

1995-06-01

Pagination or Media Count:

109.0

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 chargercontroller 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.

Subject Categories:

  • Aircraft
  • Electrochemical Energy Storage

Distribution Statement:

APPROVED FOR PUBLIC RELEASE