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SAE AIR 65:2018-05-03

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SAE AIR 65:2018-05-03

Thermoelectric Circuits and the Performance of Several Aircraft Engine Thermocouples

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The NET EMF of a thermoelectric circuit can be thought of as originating entirely in the regions of temperature gradient. Any extraneous materials, such as switch or connector terminals, in a temperature gradient may cause an error in the temperature measurement. In addition to circuitry errors, jet engine thermocouple indications require correction for the effects of conduction, radiation, response rate, and gas velocity. The magnitudes of the corrections depend on the thermocouple design and the environmental conditions. Performance curves for several typical jet engine thermocouples are presented, with the methods of making the various corrections.

Author SAE
Editor SAE
Document type Standard
Format File
Cancellation date 2018-05-03
Confirmation date 2018-05-03
ICS 49.060 : Aerospace electric equipment and systems
Number of pages 34
Replaced by SAE AIR 65 (2018-05-03)
Set AEROPAKS10U-10
Year 2018
Document history SAE AIR 65 (2018-05-03)
Country USA
Keyword SAE 65;SAE AIR65;SAE AIR65;SAE AIR 65