An aircraft propulsion system (10) comprises an engine (12), a propeller drive shaft (14) drivingly engaged with the engine (12), a propeller (16) for propelling an aircraft and a fan (22) driving cooling air along a flow path in thermal communication with the engine (12). The engine (12) may be an internal combustion engine or other engine type having heat rejection requirements and the fan (22) may facilitate cooling of the engine (12). The propulsion system may have a pusher configuration.
AIRCRAFT PROPULSION SYSTEM WITH PROPELLER AND COOLING FAN
FLUGZEUGANTRIEBSSYSTEM MIT PROPELLER UND KÜHLGEBLÄSE
SYSTÈME DE PROPULSION D'AÉRONEF À HÉLICE ET VENTILATEUR DE REFROIDISSEMENT
06.03.2024
Patent
Elektronische Ressource
Englisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES |
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