发明名称 |
Landing Load Monitor for Aircraft Landing Gear |
摘要 |
A landing gear monitor for aircraft landing gear including a plurality of pairs of wheels on a bogie, in which the main strut oil pressure serves to indicate landing load and is monitored in relation to, respectively, the two-wheel mode and the four-wheel mode, the two-wheel mode being the condition when a first of the plurality of pairs of wheels on the bogie contacts the ground and the four-wheel mode being the condition of a first and a second of the plurality of pairs of wheels on the bogie being in full contact with the ground.
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申请公布号 |
US2010161174(A1) |
申请公布日期 |
2010.06.24 |
申请号 |
US20060989785 |
申请日期 |
2006.08.23 |
申请人 |
YATES MICHAEL STUART;KEEN PHILIP |
发明人 |
YATES MICHAEL STUART;KEEN PHILIP |
分类号 |
G01M17/00;B64C25/00;G01G19/07 |
主分类号 |
G01M17/00 |
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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