• DocumentCode
    43399
  • Title

    Simulation Analysis of the Temperature Field in an Induction Launcher

  • Author

    Li San-Qun ; Guan Xiao Cun ; Lei Bin ; Li Zhi-Yuan

  • Author_Institution
    Shijiazhuang Mech. Eng. Coll., Shijiazhuang, China
  • Volume
    41
  • Issue
    5
  • fYear
    2013
  • fDate
    May-13
  • Firstpage
    1055
  • Lastpage
    1060
  • Abstract
    Induction coil guns are a class of launchers that utilize electromagnetic energy to promote the armature. During launching, the driving coil and the armature will generate a lot of heat which can make the drive coil and the armature melt, thereby affecting the normal work of the entire induction coil gun. However, it is quite difficult to accurately describe the temperature variation of the induction coil gun because of the complexity of its structure. So, the temperature of the launcher is analyzed using the finite element method in this paper. The launcher temperature simulation model is built using ANSYS software, and the temperature distribution of the drive coil and armature is analyzed using the load transfer method. The simulation results show that, without considering magnetoresistance effect and skin effect, the temperature distribution of the drive coil is uniform; the temperature rise of the armature is mainly on the outer surface and in the tail. Finally, the launcher temperature measurement experimental platform is set up and the temperatures of key points are measured, thereby verifying the simulation results.
  • Keywords
    electromagnetic launchers; finite element analysis; magnetoresistance; temperature measurement; ANSYS software; armature melt; drive coil; driving coil; electromagnetic energy; finite element method; induction coil guns; induction launcher; load transfer method; magnetoresistance effect; skin effect; temperature distribution; temperature field; temperature measurement; temperature simulation; temperature variation; Coils; Conductivity; Heating; Plasma temperature; Temperature distribution; Temperature measurement; Thermal conductivity; Analysis; finite element method; launcher; temperature field;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/TPS.2013.2251476
  • Filename
    6512006