The present disclosure provides air cooling systems and methods for propulsion systems (e.g., aviation or aerospace propulsion systems). More particularly, the present disclosure provides integrated air cooling systems and methods utilizing air cycle machine cooling for hybrid-electric aircraft or aerospace propulsion systems or the like. The present disclosure provides integrated air cycle machine cooling into the hybrid propulsion system (e.g., into the wing-mounted hybrid propulsion system). As such, the air cooling systems and methods of the present disclosure can minimize weight while improving electric motor/generator cooling.
HYBRID PROPULSION SYSTEM WITH INTEGRATED AIR-COOLING SYSTEM
HYBRIDANTRIEBSSYSTEM MIT INTEGRIERTEM LUFTKÜHLSYSTEM
SYSTÈME DE PROPULSION HYBRIDE AVEC SYSTÈME DE REFROIDISSEMENT PAR AIR INTÉGRÉ
2024-03-20
Patent
Elektronische Ressource
Englisch
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