An exhaust system for reducing infrared emissions of a rotary wing aircraft includes a manifold; an opening in the manifold, the opening configured to face upwards and away from the rotary wing aircraft; and a chimney including a wall positioned about the opening, the chimney configured to eject an emission of intermixed secondary air and engine exhaust upwards and away from the rotary wing aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Upturned exhaust system for rotary wing aircraft


    Beteiligte:

    Erscheinungsdatum :

    30.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AFT exhaust system for rotary wing aircraft

    PANTALONE III JOSEPH / DEVITO ASHLEY / CHAPKOVICH III JOHN S et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Aft exhaust system for rotary wing aircraft

    PANTALONE III JOSEPH / CHAPKOVICH III JOHN S / DEVITO ASHLEY et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Upturned exhaust system for rotary wing aircraft

    PANTALONE III JOSEPH / CHAPKOVICH III JOHN S / DEVITO ASHLEY et al. | Europäisches Patentamt | 2017

    Freier Zugriff


    Rotary wing of fixed-wing aircraft and aircraft with rotary wing

    CHEN MINGJUN / HE LIJUN / PENG JIANPING et al. | Europäisches Patentamt | 2024

    Freier Zugriff