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    • 10. 发明授权
    • Aircraft brake wheel heat shield
    • 飞机制动轮隔热罩
    • US07255208B2
    • 2007-08-14
    • US10778480
    • 2004-02-13
    • Samuel N. Rea
    • Samuel N. Rea
    • F16D65/84
    • F16D65/847F16D2065/785
    • A perforated heat shield (20) is formed of a single layer and is implemented to be positioned between an aircraft brake assembly (34) and wheel assembly (28) in order to effectively protect the wheel assembly (28) and adjacent components from excessive thermal energy generated by an operation of the brake assembly (34) and to promote the cooling of the brake assembly (34) by allowing a partial amount of the thermal energy to radiate to the wheel assembly (28) through apertures (22) provided in the heat shield (20).
    • 穿孔隔热罩(20)由单层形成,并被实施为定位在飞行器制动组件(34)和轮组件(28)之间,以便有效地保护车轮组件(28)和相邻部件免受过热 通过制动组件(34)的操作产生的能量并且通过允许部分热能通过设置在所述制动组件(34)中的孔(22)向所述车轮组件(28)辐射而促进所述制动组件(34)的冷却。 隔热罩(20)。