发明名称 |
LANDING GEAR FORCE AND MOMENT DISTRIBUTOR |
摘要 |
<p>A landing gear force and moment distributor system for an aircraft having a longitudinal axis aligned in a forward-aft direction, a vertical axis perpendicular to the longitudinal axis, and a landing gear including a pair of bogies arranged symmetrically about the longitudinal axis, each bogie having an actuator arranged to brake and/or drive one or more wheels. The force distribution system includes a distribution module arranged to: receive an input demand including a longitudinal force input demand corresponding to a desired braking or driving force along the longitudinal axis for the landing gear and a moment input demand corresponding to a desired moment about the vertical axis for the landing gear; and to use the received input demand to calculate an output command including, for each bogie, a longitudinal force output command corresponding to a braking or driving force along the longitudinal axis to be applied to the bogie</p> |
申请公布号 |
EP2920070(A1) |
申请公布日期 |
2015.09.23 |
申请号 |
EP20130792963 |
申请日期 |
2013.11.15 |
申请人 |
AIRBUS OPERATIONS LIMITED;AIRBUS OPÉRATIONS SAS |
发明人 |
GAMA-VALDEZ, MIGUEL ANGEL;ROMANA, LOUIS-EMMANUEL;DAMIANI, ANDREA;WHINCUP, MICHAEL RICHARD |
分类号 |
B64C25/40;B60T8/17;B64C25/48 |
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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