An aircraft propulsion system (1300) includes a fan (602), a primary powerplant (606), an augmenting powerplant (608) and a controller (610). The primary powerplant (606) is coupled to the fan (602) and configured to rotate the fan (602) during a first flight stage and during a second flight stage. The augmenting powerplant (608) is coupleable with the fan (602). The controller (610) is configured to cause the augmenting powerplant (608) to drive the fan (602) during the first flight stage, and to cause the augmenting powerplant (608) to cease driving the fan (602) based on an indication of a transition from the first flight stage to the second flight stage.


    Access

    Download


    Export, share and cite



    Title :

    СИСТЕМА И СПОСОБ ДЛЯ ФОРСИРОВАНИЯ ГЛАВНОЙ СИЛОВОЙ УСТАНОВКИ


    Publication date :

    2019-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge