• DocumentCode
    2907104
  • Title

    Advances in passive PCB thermal control

  • Author

    Pergande, Albert ; Rock, Janice C.

  • Author_Institution
    Lockheed Martin, Orlando, FL, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    In this paper, the author discusses the use of carbon composites, metal carbon composites and two types of carbon Nanopapers in Printed Circuit boards as a thermal control method. The emphasis is on directly mounting active power components on the thermal control layer to minimize cost and assembly complexity. Metal carbon composites, Bucky paper and Long Wall Carbon nanomaterials were acquired from commercial vendors and processed through a commercial PCB facility. A number of issues were confronted and solved to make these materials compatible with PCB fabrication, and all are now potentially available for use in military or commercial systems. The resultant PCB´s were then thermally tested and modeled to give in-situ thermal performance. Measured and predicted thermal conductivity for commercial products was excellent, giving confidence that the measured number for the carbon material is accurate. Given that carbon papers have not been optimized for thermal conductivity, there exists a significant potential for even better performance in the near future.
  • Keywords
    carbon; nanostructured materials; printed circuits; thermal conductivity; active power components; bucky paper; carbon composites; carbon nanopapers; commercial PCB facility; commercial products; long wall carbon nanomaterials; metal carbon composites; passive PCB thermal control; printed circuit boards; thermal conductivity; thermal control layer; thermal control method; Carbon; Conductivity; Copper; Heating; Materials; Radio frequency; Thermal conductivity;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747312
  • Filename
    5747312