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Cooling of Avionic Equipment by Thermoelectric Methods

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1 Author(s)
E. P. Little ; Aircraft Division Douglas Aircraft Company, Inc.

This paper presents the results of a study conducted to determine the use of a centralized thermoelectric cooling system to provide cooling for military avionic equipment. The system considered is a recirculatory system capable of cooling an avionic equipment compartment or a number of avionic equipment components from the centralized cooler. The results of the study indicate that the system is competitive on a weight basis with respect to contemporary subsonic avionic cooling systems in the range of from 2 to 4 kilowatts cooling capacity and that the system presents many attractive features for avionic equipment cooling.

Published in:

IEEE Transactions on Aerospace  (Volume:2 ,  Issue: 2 )