发明名称 FAILURE STOP MECHANISM IN STABILIZER DRIVE
摘要 PROBLEM TO BE SOLVED: To provide a stabilizer drive for guaranteeing the continuous operation via a sub-shaft when a serious failure such as breakage of a main shaft device for transmitting the steering force of an aircraft steering system. SOLUTION: The stabilizer drive has a main shaft device consisting of a cylindrical screw rod with a ball screw formed on an outer circumference, and a nut screwed to the screw rod via a ball, and is provided with an interlocking mechanism for interlocking the operation of the nut in the main shaft device with a wing of an aircraft. The stabilizer driving device comprises a sub-shaft inserted in the screw rod for rotatably holding the screw rod, a detection mechanism for detecting the breakage of the screw rod or a housing when they are broken, and a restriction mechanism for restricting the main shaft device by the sub-shaft by integrally coupling the main shaft device and the sub-shaft with each other by the operation of the detection mechanism. A failure stop mechanism in a stabilizer driving device immediately stops the tail steering force, and ensures the flight safety by mechanically stopping and holding the tail angle at the position immediately after the failure. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2007076573(A) 申请公布日期 2007.03.29
申请号 JP20050269479 申请日期 2005.09.16
申请人 SHIMADZU CORP 发明人 MURAKAMI HIROAKI
分类号 B64C13/00 主分类号 B64C13/00
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