An optical sensing system based on a micromachined silicon resonator h
as been developed and has been successfully field tested in a harsh ae
rospace environment. Two vibrating silicon beams mounted above a diaph
ragm are addressed by the same optical fibre. As pressure is applied,
the diaphragm generates stress changing the resonance frequency of a b
eam clamped at both ends. Additionally, a cantilever beam is located v
ery close to the first beam which is only sensitive to the ambient tem
perature. Detailed investigations were undertaken to obtain a better i
nsight into the photothermal activation and interferometric detection
of the resonating beams. The sensor itself was fabricated from monocry
stalline silicon using silicon to silicon fusion bonding and electro-c
hemical etch stop techniques. For packaged sensors with a pressure ran
ge from zero to 130 kPa or 3 MPa an overall accuracy of 0.05% full sca
le was achieved.