Optical pressure and temperature sensors for aerospace applications

Author:

Pinnock Robert A.

Abstract

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.

Publisher

Emerald

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering

Reference3 articles.

1. Culshaw, B. (1989, “Applications of fiber optic sensors in the aerospace and marine industries”, in Optical Fiber Sensors: Systems and Applications, Vol. 2, Artech House, Norwood, MA, pp. 701‐04.

2. Jacobs‐Cook, A.J., “Signal retrieval arrangement for vibrating sensor”, European Patent Application EP073888..

3. Jacobs‐Cook, A.J. and Bowen, M.E.C. (1993, “Novel optical fibre/microresonator interfacing technology”, Sensors and Actuators A, Vol. 37‐8, pp. 540‐45.

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