发明名称 |
Drive system for landing gear and drive system control method |
摘要 |
A method for controlling a separation between rotational axes of a pair of meshing gears 64,66 is disclosed. A parameter indicative of a transmission error through the gears is measured and the separation is controlled by an actuator 58 in order to minimise variations in the measured signal. This acts to reduce variations in transmission error and the related vibrations created in the drive system and in the surrounding components. A related drive system and aircraft landing gear are described. |
申请公布号 |
GB2523847(A) |
申请公布日期 |
2015.09.09 |
申请号 |
GB20140004699 |
申请日期 |
2014.03.17 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
FRASER WILSON |
分类号 |
B64C25/40;F16H1/26;F16H57/00;F16H57/022 |
主分类号 |
B64C25/40 |
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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