• DocumentCode
    2109348
  • Title

    Thermo-mechanical analysis of MEMS pressure sensor die-attach for high temperature applications

  • Author

    Meyyappan, Karumbu ; McCluskey, Patrick ; Chen, LiangYu

  • Author_Institution
    CALCE EPSC, Maryland Univ., College Park, MD, USA
  • Volume
    4
  • fYear
    2004
  • fDate
    13-13 March 2004
  • Firstpage
    2556
  • Abstract
    The thermomechanical stress generated by the mismatch of the coefficients of thermal expansion (CTE) of the sensor base material (SiC) and the packaging has a significant impact on the reliability of the packaged sensor. In the current work, non-linear finite element analysis was performed to determine the peeling, shear stresses and the von Mises stresses, in the SiC pressure sensor and the die attach which is intended for high temperature operation. A parametric study has been conducted to study the effects of the substrate material and reference (stress-free) temperature.
  • Keywords
    chip scale packaging; finite element analysis; high-temperature electronics; microassembling; microsensors; pressure sensors; reliability; silicon compounds; thermal expansion; thermal management (packaging); thermal stresses; wide band gap semiconductors; AlN; MEMS pressure sensor; SiC; SiC pressure sensor; coefficients of thermal expansion; die attach; high temperature applications; nonlinear finite element analysis; packaged sensor; peeling; reference temperature; reliability; sensor base material; shear stresses; substrate material effect; thermomechanical analysis; thermomechanical stress; von Mises stresses; Finite element methods; Materials reliability; Micromechanical devices; Packaging; Silicon carbide; Temperature sensors; Thermal expansion; Thermal sensors; Thermal stresses; Thermomechanical processes;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2004. Proceedings. 2004 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-8155-6
  • Type

    conf

  • DOI
    10.1109/AERO.2004.1368049
  • Filename
    1368049