发明名称 |
POSITION SENSOR SYSTEM FOR A LANDING GEAR ASSEMBLY AND METHOD OF MONITORING |
摘要 |
A position sensor system for a landing gear assembly includes a cylinder operatively coupled to an aircraft. Also included is a piston configured to translate within the cylinder. Further included is a pattern disposed on an outer surface of the piston. Yet further included is a scanner operatively coupled to the cylinder and positioned to optically detect the pattern during translation of the piston. Also included is a microprocessor in operative communication with the scanner and configured to receive data from the scanner for conversion to a quantity of movement of the piston relative to the cylinder. |
申请公布号 |
WO2016061323(A1) |
申请公布日期 |
2016.04.21 |
申请号 |
WO2015US55694 |
申请日期 |
2015.10.15 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
CLARKE, CHARLES W. |
分类号 |
G01B11/14;G01M17/04 |
主分类号 |
G01B11/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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