• DocumentCode
    1281971
  • Title

    Power management and distribution system for a more-electric aircraft (MADMEL)

  • Author

    Maldonado, M.A. ; Korba, G.J.

  • Author_Institution
    AFRL/PRPS, Wright-Patterson AFB, OH, USA
  • Volume
    14
  • Issue
    12
  • fYear
    1999
  • fDate
    12/1/1999 12:00:00 AM
  • Firstpage
    3
  • Lastpage
    8
  • Abstract
    A five-phase Power Management and Distribution System for a More-Electric Aircraft (MADMEL) program was awarded by the Air Force to Northrop/Grumman Military Aircraft Division in September 1991. The objective of the program is to design, develop, and demonstrate an advanced electrical power generation and distribution system for a More-Electric Aircraft (MEA). The MEA emphasizes the use of electrical power in place of hydraulics, pneumatic, and mechanical power to optimize the performance and life cycle cost of the aircraft. This paper presents an overview of the MADMEL program and a top-level summary of the program results, development and test of major components to date. In Phase I and Phase II studies, the electrical load requirements were established and the electrical power system architecture was defined for both near-term (NT-year 1996) and far-term (FT-year 2003) MEA application. The detailed design and specification for the Electrical Power System (EPS), its interface with the Vehicle Management System, and the test set-up were developed under Phase III. Phase IV, fabrication and testing of the subsystem level hardware, has been completed. Overall system level integration and testing, Phase V, is scheduled to be completed by September 1999
  • Keywords
    DC-AC power convertors; DC-DC power convertors; aircraft power systems; electric vehicles; invertors; military aircraft; DC-AC inverters; DC-DC converters; advanced system; battery system; electrical load requirement; electrical power system architecture; more-electric aircraft; optimized performance; power management and distribution system; subsystem testing; system level integration; vehicle management system interface; Cost function; Energy management; Fabrication; Load management; Military aircraft; Power generation; Power system management; Power systems; System testing; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.811084
  • Filename
    811084