A system for cooling a motor (24) operating within an aircraft system includes an enclosure (30) receiving ram air from a first ram air duct (44) and discharging ram air to a second ram air duct (88) to form a cooling path. The second ram air duct is discrete and independent from the first ram air duct. The system can discharge ram air between a heat exchanger (94) and a fan (96) within the second ram air duct that define a reduced or negative pressure region within the second ram air duct.
COMPONENT COOLING AND COOLING AIR FLOW GENERATION FROM REMOTE HEAT EXCHANGER
ERZEUGUNG EINES KOMPONENTENKÜHL- UND -KÜHLLUFTSTROMS AUS EINEM FERNWÄRMETAUSCHER
GÉNÉRATION DE FLUX D'AIR DE REFROIDISSEMENT ET DE REFROIDISSEMENT DE COMPOSANT À PARTIR D'ÉCHANGEUR DE CHALEUR DISTANT
2023-07-26
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
COMPONENT COOLING AND COOLING AIR FLOW GENERATION FROM REMOTE HEAT EXCHANGER
Europäisches Patentamt | 2023
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