Method and apparatus for cooling sensors in high temperature env

Measuring and testing – Vibration – By mechanical waves

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G01N 2928

Patent

active

054507537

ABSTRACT:
Sensor assemblies, comprising one or more sensors for use in high-temperature environments such as an aircraft wing, include a thermally conductive retaining member in thermal communication with either the sensor or the environment surrounding the sensor. A housing assembly placed proximate to, and in thermal communication with, the retaining member defines a fluid passageway. During operation, fluid circulates through the housing to enhance the transfer of heat away from the sensor. Such heat transfer facilitates maintaining a sensor environment within the tolerance range of the sensor, thereby facilitating monitoring of the pressure fluctuation (or other sensor parameter) during operation of the aircraft.

REFERENCES:
patent: 4175442 (1979-11-01), Terry
patent: 4295373 (1981-10-01), Moffatt
patent: 4483195 (1984-11-01), Brown
patent: 5054321 (1991-10-01), Horvath

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