发明名称 |
AIRCRAFT LANDING GEAR ARRANGEMENT, A KIT THEREFOR, AN AIRCRAFT COMPRISING THE SAME AND A METHOD OF DETERMINING THE ANGULAR POSITION OF AN AIRCRAFT WHEEL |
摘要 |
<p>An aircraft landing gear arrangement is provided comprising: . a first landing gear portion (2) comprising one or more wheels, . a second landing gear portion (3), the first landing gear portion being rotatable with respect to the second landing gear portion; and . a sensor for determining a rotational position of the first landing gear portion in relation to the second landing gear portion, . the sensor comprising a first magnetic field generator (5) operable to generate a magnetic field and a first magnetic field modulator (7) for modulating said magnetic field, . the sensor being operable to sense the magnetic field as modulated by the first magnetic field modulator (7), . the first landing portion (2) comprising the first magnetic field generator (5) or the first magnetic field modulator (7), . the second landing gear portion (3) comprising the other the first magnetic field generator (5) and the first magnetic field modulator (7).</p> |
申请公布号 |
WO2013179026(A1) |
申请公布日期 |
2013.12.05 |
申请号 |
WO2013GB51417 |
申请日期 |
2013.05.29 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
WILSON, FRASER;HAIKNEY, DAVID;HOWARD, MARK;KREIT, DARRAN |
分类号 |
B64C25/50 |
主分类号 |
B64C25/50 |
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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