The aircraft thrust control system comprises a central power unit and peripheral power units. The central power unit comprises upper and lower propellers arranged one above the other and adapted to rotate in opposite directions, while propellers of the peripheral power units are located outside the aerodynamic operating range of the central power unit propellers.


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    Title :

    AIRCRAFT THRUST AND CONTROL SYSTEM


    Additional title:

    SCHUB- UND STEUERSYSTEM FÜR FLUGZEUGE
    SYSTÈME DE POUSSÉE ET DE CONTRÔLE DES AVIONS


    Contributors:

    Publication date :

    2025-02-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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