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公开(公告)号:US10919642B2
公开(公告)日:2021-02-16
申请号:US15888120
申请日:2018-02-05
Applicant: AIRBUS OPERATIONS LIMITED
Inventor: Christopher Papadopoulos , Matthew Marples , Andy Mounty , Costas Fanourakis , Graham King
IPC: B64D45/00 , B64C25/22 , B64C25/34 , F15B15/14 , F15B19/00 , B64F5/60 , F15B1/24 , B64C25/58 , B64C13/48 , F15B1/08
Abstract: A landing gear system for an aircraft includes a retractable landing gear assembly, a hydraulic actuator for actuating movement part, for example a bogie of the landing gear assembly, and an accumulator associated with the actuator. The accumulator comprises a volume of pressurised gas separated from hydraulic fluid by a separator piston. Travel of the separator piston beyond a certain position is indicative of a fault. The accumulator includes a snubbing device that acts to slow movement of the separator piston beyond that position. A monitoring system measures the time taken for the movement of the landing gear part effected by the hydraulic actuator. If the measured time is longer than a threshold time, that is indicative of a possible fault in the accumulator, that might, without the snubbing, remain undetected and/or hidden from view.
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公开(公告)号:US09424391B2
公开(公告)日:2016-08-23
申请号:US13623977
申请日:2012-09-21
Inventor: Christopher Papadopoulos , Antonella Cavallo , Alessandro Cimatti , Marco Bozzano
CPC classification number: G06F17/50 , G06F17/5095 , G06F2217/02 , G06F2217/06 , G06F2217/08
Abstract: A computer-implemented method for determining a configuration of a plurality of components in a systems installation which satisfies one or more constraints.
Abstract translation: 一种用于确定满足一个或多个约束的系统设备中的多个组件的配置的计算机实现的方法。
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