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
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