• DocumentCode
    2273268
  • Title

    Aircraft electrical power systems prognostics and health management

  • Author

    Keller, Kirby ; Swearingen, Kevin ; Sheahan, Jim ; Bailey, Mike ; Dunsdon, Jon ; Przytula, K. Wojtek ; Jordan, Brett

  • Author_Institution
    The Boeing Co., St. Louis, MO
  • fYear
    0
  • fDate
    0-0 0
  • Abstract
    Military and commercial aircraft, spacecraft and ground vehicles are increasingly dependent on electrical power. It has become common place for vehicles to rely on electrical power, in whole or in part, for all systems, including critical systems such as flight control and fuel delivery. Microprocessors embedded in digitally controlled power distribution systems, as well as in the digital controllers within these systems, provide an unprecedented, affordable and inherent opportunity to monitor an electrically powered vehicle´s systems health. Data transmitted to and from these controllers can be used to characterize the system and component operating signatures, thereby enabling advanced diagnostic and prognostic capabilities. These capabilities will ensure a high mission reliability rate as well as reduce life cycle ownership costs. The aircraft electrical power systems prognostics and health management (AEPHM) program, presently being worked by Air Force Research Laboratories (AFRL), Boeing, and Smiths Aerospace, has developed and demonstrated health management (diagnostics, prognostics and decision aids) algorithms. The first phase of the program, which ended in July of 2005, addressed electric actuation, fuel pumps/valves and arc fault protection. The second phase is addressing power generation. Algorithm development is based on data collected from seeded and accelerated run-to-failure laboratory testing. The AEPHM architecture supports system level fusion of evidence and state information from multiple sources to improve estimates of degradation. The robustness of health management as a function of possible data sources and data rates is being determined. The product of the research will be adaptable to a range of platforms, including military, space and commercial vehicles. Phase I of the program was completed with an end to end, hardware-in-the-loop (electric actuator, fuel pump, fuel valve, arc fault, and power distribution unit) demonstration with on-line - - data generation to show the integration of the technology into a realistic setting
  • Keywords
    aerospace engineering; aircraft maintenance; aircraft power systems; avionics; control engineering computing; vehicles; AEPHM program; AFRL; Air Force Research Laboratories; Smiths Aerospace; aircraft electrical power systems; arc fault protection; commercial vehicles; electric actuation; fuel pumps/valves protection; hardware-in-the-loop; prognostics and health management; Control systems; Digital control; Fuels; Laboratories; Military aircraft; Power distribution; Power system management; Power system reliability; Prognostics and health management; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2006 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-9545-X
  • Type

    conf

  • DOI
    10.1109/AERO.2006.1656087
  • Filename
    1656087