• DocumentCode
    59685
  • Title

    Liquid Jet Impingement Cooling of a Silicon Carbide Power Conversion Module for Vehicle Applications

  • Author

    Gould, Kyle ; Cai, Steve Q. ; Neft, Charles ; Bhunia, Avijit

  • Author_Institution
    Teledyne Sci. Co., Thousand Oaks, CA, USA
  • Volume
    30
  • Issue
    6
  • fYear
    2015
  • fDate
    Jun-15
  • Firstpage
    2975
  • Lastpage
    2984
  • Abstract
    Thermal management of power electronics is an extremely challenging problem in the harsh environment of military hybrid vehicles, where the local air and liquid coolant´s temperature exceed 100 °C under regular operating conditions. This paper presents the development work of a high heat flux, jet impingement-cooled heat exchanger for a 600-V/50-A silicon carbide (SiC) power module (rated at 175 °C device junction temperature), used for bidirectional power conversion between a 28-V battery and a 300-V dc bus. A total of 50 volume% mixture of water-ethylene glycol (WEG) coolant at 100 °C inlet temperature is the only available coolant. An array of WEG coolant microjets impinges on the base plate of the SiC module. The jet impingement cooling system has been optimized by experimental studies on a surrogate module, along with a high-fidelity computational model, to accurately estimate the SiC device junction temperature in relevant operating conditions. Results indicate that at the design heat load of 151 W (worst-case scenario), the SiC device junction temperature is reduced from 290 °C with commercial-off-the-shelf (COTS) cold plate cooling and 215 °C with COTS microchannel heat exchanger cooling, to 169 °C with a jet impingement-cooled heat exchanger, using the same flow rate.
  • Keywords
    electric vehicles; heat exchangers; power conversion; silicon compounds; COTS microchannel heat exchanger cooling; SiC; WEG coolant microjets; base plate; bidirectional power conversion; commercial-off-the-shelf cold plate cooling; current 50 A; dc bus; flow rate; heat load design; high heat flux; high-fidelity computational model; liquid jet impingement cooling; military hybrid vehicles; power 151 W; power electronics; surrogate module; temperature 100 degC; temperature 169 degC; temperature 175 degC; temperature 215 degC; temperature 290 degC; thermal management; voltage 600 V; water-ethylene glycol coolant; Cold plates; Coolants; Heating; JFETs; Silicon carbide; Temperature measurement; Cooling; dc???dc power conversion; high temperature; silicon carbide (SiC); vehicle operation;
  • fLanguage
    English
  • Journal_Title
    Power Electronics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0885-8993
  • Type

    jour

  • DOI
    10.1109/TPEL.2014.2331562
  • Filename
    6838986