• DocumentCode
    1589205
  • Title

    Design of an electrical distribution test rig for validation of equipment for more electrical aircraft

  • Author

    Bester, Jean Ernst ; Mpanda, A. ; Polfliet, Niels ; Van den Keybus, Jeroen ; Hazemeyer, Guillaume Martial

  • Author_Institution
    ESIEE-Amiens, Amiens, France
  • fYear
    2013
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    In order to mitigate economical, ecological and technological challenges aircraft manufacturers have shifted towards more electrical aircraft, bringing with it many new technologies to be implemented and a redesign of the existing electrical network. This paper details the development of an electrical distribution centre as taking place under the European Framework 7 Clean Sky Program. The developed distribution centre is to be integrated into an existing electrical test bench which recreates the entire electrical system of an aircraft and allows both aircraft and aerospace equipment manufactures to conduct verification activities over different aircraft electrical architectures. The task then of the distribution centre is to bring an element of flexibility to the existing electrical test bench in order for it to be easily reconfigured into any aircraft architecture, including both airplane and rotorcraft. In order to achieve this, the distribution centre contains both low voltage and high voltage DC bus bars. The connection of sources and loads to the bus bars, and the interconnection between bus bars themselves, are achieved by using Racks, each of which contains a controllable and sequenceable switching element together with high fidelity proprietary measurement instrumentation and embedded protection. The entire system has undergone in-house testing and successfully passed factory acceptance tests before its delivery and subsequent commissioning, with the results being noted and discussed here.
  • Keywords
    aircraft power systems; aircraft testing; busbars; electric vehicles; aerospace equipment; aircraft electrical architectures; aircraft manufacturers; airplane; distribution centre; electrical aircraft system; electrical distribution test rig design; electrical network; embedded protection; equipment validation; factory acceptance tests; high fidelity proprietary measurement instrumentation; high voltage DC busbars; in-house testing; racks; rotorcraft; switching element; Aerospace electronics; Aircraft; Aircraft manufacture; Aircraft propulsion; Bars; Engines; HVDC transmission; Aerospace; Distribution of electrical energy; Energy system management; HVDC; Measurements;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Electronics and Applications (EPE), 2013 15th European Conference on
  • Conference_Location
    Lille
  • Type

    conf

  • DOI
    10.1109/EPE.2013.6634713
  • Filename
    6634713