1 August 1992 Optical micromachined pressure sensor for aerospace applications
Diogenes Thomas Angelidis, Philip J. Parsons
Author Affiliations +
Abstract
An optical pressure sensor has been designed using silicon micromachining technology. A resonant silicon beam is mounted above a diaphragm and its resonant frequency changes with applied pressure. The sensor is temperature compensated by way of a second pressure-insensitive resonator. Both resonators are optically addressed via the same optical fiber. The sensor is designed to give an overall accuracy of 0.05% full-scale pressure, which is currently between 130 kPa or 3 MPa. Optical technology allows the optical pressure sensor to operate in a harsh aerospace environment where electronic pressure sensors cannot survive.
Diogenes Thomas Angelidis and Philip J. Parsons "Optical micromachined pressure sensor for aerospace applications," Optical Engineering 31(8), (1 August 1992). https://doi.org/10.1117/12.58838
Published: 1 August 1992
Lens.org Logo
CITATIONS
Cited by 20 scholarly publications and 14 patents.
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Sensors

Silicon

Resonators

Signal detection

Aerospace engineering

Optical fibers

Micromachining

RELATED CONTENT

MEMS/NEMS development for space applications at NASA/JPL
Proceedings of SPIE (April 19 2002)
Optically Activated Resonator Sensors
Proceedings of SPIE (January 03 1986)
CMOS resonant sensors
Proceedings of SPIE (September 08 1998)

Back to Top