The present disclosure is a heat radiator for an aircraft which cools a heat source installed in the aircraft, which includes a heat radiating part in which a contact surface comes into contact with a main flow, the contact surface being formed with a concave portion or a convex portion in which a surface thereof directed upstream in a flow direction of the main flow is curved in a plan view.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HEAT RADIATOR FOR AIRCRAFT


    Beteiligte:
    OKITA YOJI (Autor:in) / MURATA AKIRA (Autor:in)

    Erscheinungsdatum :

    2019-08-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    HEAT RADIATOR FOR AIRCRAFT

    OKITA YOJI / MURATA AKIRA | Europäisches Patentamt | 2018

    Freier Zugriff

    HEAT RADIATOR FOR AIRCRAFT

    OKITA YOJI / MURATA AKIRA | Europäisches Patentamt | 2020

    Freier Zugriff

    RADIATOR FOR AIRCRAFT

    Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPELLER BLADE RADIATOR

    MANNING KERRY GREGG | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft propeller blade radiator

    MANNING KERRY GREGG | Europäisches Patentamt | 2024

    Freier Zugriff