An improved air-cooled aviation engine includes a compact combustion chamber having an intake valve opening, an exhaust valve opening, and a generally elliptical shape. The elliptical shape has a major axis and a minor axis, with the major axis intersecting both the intake valve opening and the exhaust valve opening. In some examples, the major axis is the same length or shorter than a diameter of a cylinder bore of the engine, and the minor axis is smaller than the major axis. Combustion is thus constrained to a smaller area than that of the cylinder bore.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIR-COOLED, FOUR-STROKE AVIATION ENGINE


    Beteiligte:

    Erscheinungsdatum :

    09.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02F CYLINDERS, PISTONS, OR CASINGS FOR COMBUSTION ENGINES , Zylinder, Kolben oder Gehäuse für Brennkraftmaschinen / F01L CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES , Periodisch betriebene Ventile für Kraft- und Arbeitsmaschinen oder Kraftmaschinen



    AIR-COOLED, FOUR-STROKE AVIATION ENGINE

    BAER PATRICK HENRY / GLUCKSMAN MICHAEL GLYNN | Europäisches Patentamt | 2024

    Freier Zugriff

    Air-cooled, four-stroke aviation engine

    BAER PATRICK HENRY / GLUCKSMAN MICHAEL GLYNN | Europäisches Patentamt | 2024

    Freier Zugriff

    Oil-cooled four-stroke engine for power paragliding

    WEN WENXIAN | Europäisches Patentamt | 2023

    Freier Zugriff