Liquid-Cooled Aircraft Electronic Systems

Liquid cooling systems provide superior localized cooling compared to air or gas cooling.

Compared to air or gas, liquids achieve a much higher heat transfer coefficient.

This results in smaller temperature differences between component temperatures and coolant supply temperatures.

A smaller temperature gradient allows components to operate at lower temperatures.

This increases component reliability and reduces maintenance costs.

The higher heat transfer coefficients of liquid cooling systems allow adequately cooling higher power densities.

In addition, liquids cool low power density equipment more efficiently than air cooling.

However, the disadvantages of liquid cooling systems must also be analyzed for any potential application.

Key considerations include maintenance, potential leakage, fluid contamination, logistics, and fire hazards.

Direct Liquid Cooling:
The liquid can be used to remove heat directly from the heat source.
This provides minimal thermal resistance between the heat source and the liquid.

Indirect Liquid Cooling:
In this method, heat is transferred to the liquid in a liquid-cooled cold plate through an intermediate device.

With engineering, manufacturing, and testing capabilities compliant with aviation standards in both air and liquid cooling technologies, TASECS ensures the reliability, performance, and mission continuity of aircraft electronic systems.