The invention belongs to the technical field of aviation brake aircraft wheels, and particularly relates to an integral heat shield for an aviation brake aircraft wheel. Comprising an inner heat insulation screen, an outer heat insulation screen, a heat insulation layer, a plurality of isolation pads and a plurality of reinforcing plates. The heat insulation layer and the inner heat insulation screen are arranged in the outer heat insulation screen, the heat insulation layer is arranged in a cavity between the inner heat insulation screen and the outer heat insulation screen and is clamped by semi-circular truncated cones on the inner heat insulation screen and the outer heat insulation screen, and the cavity is divided into two cavities; and the thermal protection area of the hub wall of the airplane wheel assembly is increased to 100%.

    本发明属于航空刹车机轮技术领域,尤其涉及一种用于航空刹车机轮的整体式隔热屏。包括:内隔热屏、外隔热屏、隔热层、多个隔离垫和多个加强板;所述隔热层和所述内隔热屏装入所述外隔热屏内,所述隔热层在所述内隔热屏和所述外隔热屏之间的空腔中,且被内隔热屏和外隔热屏的上的半圆台夹紧,将一个空腔隔成两个空腔;将机轮组件毂壁的热防护面积提高至100%。


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    Titel :

    Integral heat shield for aviation brake airplane wheel


    Weitere Titelangaben:

    一种用于航空刹车机轮的整体式隔热屏


    Beteiligte:
    LOU JINTAO (Autor:in) / YI ZHE (Autor:in) / DING BIN (Autor:in) / LIU GANG (Autor:in) / LI XIAOMENG (Autor:in) / CHEN YU (Autor:in) / ZHANG XIAO (Autor:in)

    Erscheinungsdatum :

    24.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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