• DocumentCode
    1880432
  • Title

    Integrated PCB active cooling with piezoelectric actuator

  • Author

    English, Brian A. ; Hudson, Tracy ; Whitley, Michael R. ; Rock, Janice ; Kranz, Michael S.

  • Author_Institution
    EngeniusMicro, LLC, Atlanta, GA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    Thermal management is challenging in RF communication and radar systems that require high-power levels for operation and reliability as well as small footprints to control intrinsic losses and meet design constraints. An interesting approach uses discrete, in-situ fluid handling and embedded synthetic jet drivers to enhance local cooling at the component. In this approach, fluid cavities and actuators are integrated into the PCB near the component. Magnetic and piezoelectric actuators have proven effective in other less-demanding applications. The challenge to adapting from magnetic to piezoelectric actuators is to achieve high flowrates because piezo-actuators have lower displacement and higher frequencies. This investigation explores frequency and displacement effects on cooling rates for piezo-actuators embedded in PCB. Further concept development includes integration with thermal ground planes.
  • Keywords
    magnetic actuators; piezoelectric actuators; printed circuit manufacture; thermal management (packaging); RF communication; cooling rates; design constraints; displacement effects; embedded synthetic jet drivers; fluid cavities; frequency effects; high-power levels; in-situ fluid handling; integrated PCB active cooling; intrinsic losses; local cooling; magnetic actuators; piezo-actuators; piezoelectric actuators; radar systems; thermal ground planes; thermal management; Cavity resonators; Cooling; Data acquisition; Heating; Orifices; Substrates; Temperature measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187089
  • Filename
    6187089