A leading edge assembly for a hypersonic vehicle is provided. The leading edge assembly includes an outer wall that tapers to a leading edge, the outer wall having a porous region at the leading edge; a coolant supply assembly in fluid communication with the porous region for selectively providing a flow of coolant through the porous region of the outer wall; and an insulation layer disposed between a portion of the coolant supply assembly and the outer wall, wherein the insulation layer is configured to reduce heat transfer between the coolant supply assembly and the outer wall.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE


    Beteiligte:

    Erscheinungsdatum :

    2023-09-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    System for cooling leading edge of high-speed vehicle

    RASSE NICHOLAS WILLIAM / NATSUY GREGORY ALEXANDER / DYSON THOMAS EARL | Europäisches Patentamt | 2023

    Freier Zugriff

    System and method for cooling leading edge of high speed vehicle

    RATHAY NICHOLAS WILLIAM / RUSH BRIAN MAGANN / NATSUI GREGORY ALEXANDER | Europäisches Patentamt | 2021

    Freier Zugriff

    System and method for cooling leading edge of high speed vehicle

    RATHAY NICHOLAS WILLIAM / NATSUI GREGORY ALEXANDER / RUSH BRIAN MAGANN | Europäisches Patentamt | 2021

    Freier Zugriff

    SYSTEM AND METHOD FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE

    RATHAY NICHOLAS WILLIAM / BOURASSA COREY / HOFER DOUGLAS CARL et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    System and method for cooling a leading edge of a high speed vehicle

    HOFER DOUGLAS CARL / RATHAY NICHOLAS WILLIAM / NATSUI GREGORY ALEXANDER et al. | Europäisches Patentamt | 2023

    Freier Zugriff