The invention relates to an application of lifting engine with self-contained aerofoils to a vertical take-off and landing aircraft. Figure 1. Application of Lifting Engine to Vertical Take-Off Aircraft - General Layout Litting Engine arbd AertOils can rotate Relative to Fuselage Low Drag Fuselage (no landing gear or additional WIt required) Liting Engine with Self-Contained Aerofoils - Motor can Rotate RelatNe to Aerofoils 1 of 2


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    Title :

    APPLICATION OF LIFTING ENGINE WITH SELF-CONTAINED AEROFOILS TO VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    Contributors:

    Publication date :

    2017-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge