• DocumentCode
    2833014
  • Title

    MEMS pressure sensors for aerospace applications

  • Author

    Lin, Liwei ; Yun, Weijie

  • Author_Institution
    Dept. of Mech. Eng. & Appl. Mech., Michigan Univ., Ann Arbor, MI, USA
  • Volume
    1
  • fYear
    1998
  • fDate
    21-28 Mar 1998
  • Firstpage
    429
  • Abstract
    MEMS (microelectromechanical systems) pressure sensors have been designed, fabricated and characterized. The fabrication process is fully compatible with IC (integrated circuit) fabrication such that multifunctional microelectronics can be directly integrated on the same chip for advanced aerospace applications. These pressure sensors are designed based on the piezoresistive sensing principle on surface micromachined polysilicon thin diaphragms. Both square- and circular-shape diaphragms with thickness of 2 μm and width (diameter) of 100 μm have been designed and fabricated. Prototype pressure sensors with 100 Psi in full scale have a measured sensitivity of 0.15 mV/V/Psi and a maximum linearity error of ±0.1% FSS (full scale span)
  • Keywords
    aircraft instrumentation; elemental semiconductors; microsensors; piezoresistive devices; pressure sensors; silicon; 100 micron; 100 psi; MEMS pressure sensors; Si; aerospace applications; circular-shape diaphragms; fabrication process; maximum linearity error; measured sensitivity; multifunctional microelectronics; piezoresistive sensing principle; polysilicon thin diaphragms; square-shape diaphragms; Application specific integrated circuits; Fabrication; Microelectromechanical systems; Microelectronics; Micromechanical devices; Piezoresistance; Pressure measurement; Prototypes; Sensor phenomena and characterization; Sensor systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1998 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-4311-5
  • Type

    conf

  • DOI
    10.1109/AERO.1998.686941
  • Filename
    686941