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.
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
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