This paper gives a brief overview of requirements within the aerospace market sector for which optical sensors are of potential benefit, and goes on to describe sensors currently under development at Lucas Electrical and Electronic Systems which are primarily intended to meet some of these requirements. These sensors, based on the combination of silicon micromachining and optical sensing technologies, are sufficiently robust to provide the capability of directly measuring on‐engine parameters such as pressure and temperature. In association with FADEC‐mounted interface units, to which the sensor heads are coupled via optical fibre links, the sensors have the potential to provide measurement data for a number of aero‐engine control requirements.
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1 March 1998
Technical Paper|
March 01 1998
Optical pressure and temperature sensors for aerospace applications
Robert A. Pinnock
Robert A. Pinnock
Principal Engineer within the Advanced Product Development Group of Lucas Electrical and Electronic Systems, Stratford Road, Solihull BD90 4GW
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Publisher: Emerald Publishing
Online ISSN: 1758-6828
Print ISSN: 0260-2288
© MCB UP Limited
1998
Sensor Review (1998) 18 (1): 32–38.
Citation
Pinnock RA (1998), "Optical pressure and temperature sensors for aerospace applications". Sensor Review, Vol. 18 No. 1 pp. 32–38, doi: https://doi.org/10.1108/02602289810198293
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