发明名称 Aircraft landing gear having axle to brake plate integration
摘要 An aircraft landing gear brake arrangement wherein a landing gear stub axle and brake pressure plate are integrated. Each of the integrated assemblies is attached to a support fitting which pivots on the truck axle thereby causing the torque links to be unaffected by steering operations.
申请公布号 US6149100(A) 申请公布日期 2000.11.21
申请号 US19980140487 申请日期 1998.08.26
申请人 THE BOEING COMPANY 发明人 RALPH, HARRY C.
分类号 B64C25/34;B64C25/42;(IPC1-7):B64C25/02 主分类号 B64C25/34
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