Liquid cooled approaches for high density avionics

Next-generation aircraft will require avionics that provide greater system performance in a smaller volume. That requires highly developed thermal management techniques. To meet this need, a liquid-cooled approach has been developed to replace the conventional air-cooled approach for high-power applications. Liquid-cooled chassis and flow-through modules have been developed to limit junction temperatures to acceptable levels. Liquid cooling also permits emergency operation after loss of coolant for longer time intervals, which is desirable for flight-critical airborne applications. Activity to data has emphasized the development of chassis and modules that support the US Department of Defense´s (DoD) two-level maintenance initiative as governed by the joint Integrated Avionics Working Group (JIAWG)