Technologies are described herein for a drag recovery scheme. In various examples, a recovery engine is placed within a vortex flow of air caused by the impingement of air upon a nacelle of a main engine. The propeller of the recovery engine can use the vortex flow of air to provide additional thrust the aircraft, thus reducing the load on the main engines or providing an increased velocity.


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    Titel :

    Drag recovery scheme for nacelles


    Beteiligte:
    PAGE MARK A (Autor:in) / WINKLER JOHN (Autor:in) / KENNELLY BRENDAN (Autor:in)

    Erscheinungsdatum :

    12.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    DRAG RECOVERY SCHEME FOR NACELLES

    PAGE MARK A / KENNELLY BRENDAN / WINKLER JOHN | Europäisches Patentamt | 2020

    Freier Zugriff

    DRAG RECOVERY SCHEME FOR NACELLES

    PAGE MARK A / WINKLER JOHN / KENNELLY BRENDAN | Europäisches Patentamt | 2020

    Freier Zugriff

    Automated Design of Minimum Drag Light Aircraft Fuselages and Nacelles

    F. O. Smetana / S. R. Fox / B. E. Karlin | NTIS | 1982


    Automated design of minimum drag light aircraft fuselages and nacelles

    Smetana, F. O. / Fox, S. R. / Karlin, B. E. | NTRS | 1982


    Drag tests of 4/9-scale model engine nacelles with various cowlings

    Windler, R. | Engineering Index Backfile | 1932