A propulsion system for an aircraft including a fuselage and a wing assembly. The propulsion system includes a first propulsion device at the level of the rear part of the fuselage and constituted of at least one BLI propulsion unit including a fan, a second propulsion device constituted of at least one conventional propulsion unit, and a transmission device coupling the first and second propulsion devices. The second propulsion system therefore generates the energy necessary for driving in rotation the fan of the BLI propulsion unit or units. The thrust produced by the propulsion devices contributes to generating the total thrust of the aircraft. In this propulsion system at least one conventional propulsion unit constituting the second propulsion device is situated on one side of the rear part of the fuselage between the tail of the fuselage and the wing assembly of the aircraft.


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    Title :

    BLI PROPULSION SYSTEM WITH THREE AFT PROPULSION UNITS


    Contributors:

    Publication date :

    2020-07-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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