An aircraft includes an airframe defining a first enclosed space, an engine bay disposed within the first enclosed space, and a cooling system. The engine bay includes a firebox defining a second enclosed space and an engine disposed at least partially within the second enclosed space. The cooling system is configured to selectively fluidly couple the first enclosed space with the second enclosed space.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AVIONIC EXHAUST AIR FOR COOLING ENGINE BAY


    Beteiligte:

    Erscheinungsdatum :

    02.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Avionic exhaust air for cooling engine bay

    ALBERTI GIUSEPPE S / CIRIOLI ADRIANO / BARROWS SEAN THOMAS et al. | Europäisches Patentamt | 2024

    Freier Zugriff


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987