Abstract A rotating propeller or fan motor, ducted or un-ducted, with two or more self-contained aerofoils connected with side supports, the aerofoils are placed within the engine slipstream so that lift is achieved as a by-product of the forward thrust, the motor is fixed to the outer side support on a rotating bracket to allow the angle of attack between the propeller slipstream and aerofoils to be adjusted. Figure 2. Side View of Lifting Engine with Self Contained Aerofoils AMI M ts bal4. . - #~nWg P43r A~enrAd iqw r4 M9e *


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    Titel :

    LIFTING ENGINE WITH SELF CONTAINED AEROFOILS


    Beteiligte:

    Erscheinungsdatum :

    15.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




    Stalling aerofoils

    Jones, M. | Engineering Index Backfile | 1934



    Stalling aerofoils

    Jones, M. | Engineering Index Backfile | 1934


    Tadem aerofoils

    Nayler, J. L. / Page, W. L. | TIBKAT | 1922