Aircraft turbine engines are controlled by complex electronic devices such as FADEC and PSS units. These devices can be adversely impacted by the engine environment including the condensing of evaporated water. Aspects of the present disclosure include unique heat exchangers to control the temperature of these electronic devices to assure their proper operation.
AVIONICS HEAT EXCHANGER
16.07.2020
Patent
Elektronische Ressource
Englisch
A High Flux Heat Exchanger for Military Avionics Part II: Test Results
British Library Conference Proceedings | 1994
|A High Flux Heat Exchanger for Military Avionics Part II: Test Results
SAE Technical Papers | 1994
|