发明名称 Aircraft landing gear
摘要 <p>Aircraft landing gear including: a bogie beam coupled to a main strut; a first and second axles mounted on the bogie beam, each axle having a respective brake assembly and wheel assembly; and first and second stabilising arms mechanically coupling the first and second brake assemblies to respective first and second anchor points on the landing gear so as to react respective first and second brake torques generated as respective brake assembly applies a braking force to the respective wheel assembly. The first and second stabilising arms couple the respective first and second brake assemblies to the respective first and second anchor points such that the first and second brake torques result in both stabilising arms experiencing a tensile force or both stabilising arms experiencing a compressive force.</p>
申请公布号 GB201106253(D0) 申请公布日期 2011.05.25
申请号 GB20110006253 申请日期 2011.04.13
申请人 MESSIER-DOWTY LIMITED 发明人
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