• DocumentCode
    540920
  • Title

    Design for fault tolerance and predictive failures

  • Author

    Wolmarans, J.J. ; Ferreira, J.A. ; Polinder, H. ; Josifovic, I. ; Clarenbach, D.

  • Author_Institution
    Delft Univ. of Technol., Delft, Netherlands
  • fYear
    2010
  • fDate
    16-18 March 2010
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    System integration and fault tolerance aims to help achieve high levels of availability and power density in aerospace applications. A 50kW integrated machine and drive with fault tolerance is described. For monitoring system health and diagnostics, an array of sensors is embedded. On state voltages and device currents are compared to ensure equal current sharing. By implementation of a power module using surface mount technology and double sided components a modular design is achieved. Key module parameters are constantly measured, through which faults can be detected and the ageing of a module may be quantified. Once a specific module has reached a predetermined age, the module may be removed from operation. The supporting system architecture will allow the remaining system to continue operation, therefore creating a fault tolerant system.
  • Keywords
    aerospace instrumentation; electric drives; electric machines; fault tolerance; sensor arrays; surface mount technology; aerospace application; double sided component; fault tolerance design; fault tolerant system; integrated machine; power 50 kW; power density; power module; predictive failures; sensor array; surface mount technology; Current measurement; Fault tolerance; Fault tolerant systems; Semiconductor device measurement; Temperature measurement; Temperature sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Integrated Power Electronics Systems (CIPS), 2010 6th International Conference on
  • Conference_Location
    Nuremberg
  • Print_ISBN
    978-1-61284-814-3
  • Type

    conf

  • Filename
    5730631