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.


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    Title :

    AIRCRAFT PROPULSION SYSTEM WITH PROPELLER AND COOLING FAN


    Additional title:

    FLUGZEUGANTRIEBSSYSTEM MIT PROPELLER UND KÜHLGEBLÄSE
    SYSTÈME DE PROPULSION D'AÉRONEF À HÉLICE ET VENTILATEUR DE REFROIDISSEMENT


    Contributors:
    DIONNE LUC (author)

    Publication date :

    2024-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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