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Invention Grant
US08087824B2 Aircraft brake assembly having a temperature probe and method of mounting a temperature probe in a brake assembly 有权
具有温度探头的飞行器制动组件和将温度探头安装在制动组件中的方法

Aircraft brake assembly having a temperature probe and method of mounting a temperature probe in a brake assembly
Abstract:
An aircraft brake assembly (10) includes a torque tube (16) having a passageway (18) for receiving a temperature probe, the passageway (18) having a wall and a width (W) and a length, and a temperature probe (20) having a width (w) less than the passageway width (W) and at least one angled portion (34, 36) where a centerline (44) of the temperature probe (20) changes direction. The temperature probe (20) has a lateral offset (L) greater than the passageway width (W) so that the probe (20) cannot be inserted into the passageway (18) without flexing it at the at least one angled portion (34, 36), and the temperature probe (20) is mounted in the passageway (18) and held in a flexed state by the passageway wall. Also a method of mounting a temperature probe in a brake assembly.
Abstract(Chinese):

飞机制动器组件（10）包括具有用于接收温度探针的通道（18）的扭矩管（16），所述通道（18）具有壁和宽度（W）和长度，以及温度探头（20 ）具有小于通道宽度（W）的宽度（w）和温度探头（20）的中心线（44）改变方向的至少一个倾斜部分（34,36）。 温度探针（20）具有大于通道宽度（W）的横向偏移（L），使得探针（20）不能插入通道（18）中，而不会在至少一个倾斜部分（34， 36），并且温度探针（20）安装在通道（18）中并且通过通道壁保持弯曲状态。 还有一种将温度探头安装在制动组件中的方法。

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