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US08127899B2 Torque pads for aircraft brake systems and aircraft brake system including same 失效
用于飞机制动系统和飞机制动系统的扭矩垫包括它们

Torque pads for aircraft brake systems and aircraft brake system including same
Abstract:
An aircraft brake system (42) includes a torque tube (44), a plurality of spaced stators (48) mounted on the torque tube (44), a wheel (40) surrounding the torque tube (44) and a plurality of rotors (50) connected to the wheel (40) and projecting into the spaces between adjacent ones of the stators (48). A backing plate (52) mounted on the torque tube (44) has a first side (54) facing the rotors (50) and a second side (56) facing away from the rotors (50), and the second side (56) includes a plurality of keyways (58). A plurality of torque pads (10, 70, 100, 120) are connected to the torque tube (44), each having a body (12, 72, 102, 122) with a first surface (14, 74, 104, 124) contacting the second side (56) of the backing plate (52) and at least one key (22, 82, 112, 114, 130, 132) projecting from the first surface (14, 74, 104, 124) into one of the plurality of keyways (58). Also a torque pad (10, 70, 100, 120) and a method of connecting a backing plate to a torque tube.
Abstract(Chinese):

飞机制动系统（42）包括扭矩管（44），安装在扭矩管（44）上的多个隔开的定子（48），围绕扭矩管（44）的轮（40）和多个转子 连接到轮（40）并突出到相邻定子（48）之间的空间中。 安装在扭矩管（44）上的背板（52）具有面向转子（50）的第一侧面（54）和背离转子（50）的第二侧面（56），第二侧面（56） 包括多个键槽（58）。 多个扭矩垫（10,70,100,120）连接到扭矩管（44），每个扭矩垫具有带有第一表面（14,74,104,124）的主体（12,72,102,122） 接触所述背板（52）的第二侧（56）和从所述第一表面（14,74,104,124）突出的至少一个键（22,82,112,114,130,132）到所述第一表面 多个键槽（58）。 还有一个扭矩垫（10,70,100,120）以及将背板连接到扭矩管的方法。

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