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    • 6. 发明授权
    • Aircraft landing gear
    • 飞机起落架
    • US06948683B2
    • 2005-09-27
    • US10899766
    • 2004-07-27
    • Michel DerrienBenjamin Parzy
    • Michel DerrienBenjamin Parzy
    • B64C25/10
    • B64C25/10B64C2025/345
    • An aircraft landing gear includes a leg having a strut receiving a telescopic rod to slide on a sliding axis, the strut being hinged to an aircraft structure and being capable of pivoting about a pivot axis that is highly offset from the sliding axis. The landing gear further includes a connection structure essentially formed by two panels connecting two axially separate points of the strut to a common axis structure extending along the strut pivot axis. In the gear-down position, the panels are one above the other, the top panel being connected to the strut via a high attachment which is rigid in twisting, while the bottom panel is connected to the strut via a low attachment which tolerates twisting, thereby enabling the strut to warp to some extent when the aircraft is turning while taxiing.
    • 飞机起落架包括具有支撑杆的支腿,所述支柱接收伸缩杆以在滑动轴线上滑动,所述支柱铰接到飞行器结构并且能够围绕与所述滑动轴线高度偏移的枢转轴线枢转。 起落架进一步包括连接结构,该连接结构主要由将支柱的两个轴向分离的点连接到沿着支柱枢转轴线延伸的公共轴线结构的两个面板形成。 在减速位置中,面板是彼此之一的,顶板通过刚性扭转的高附件连接到支柱,而底板通过低附件连接到支柱,该附件允许扭转, 从而使得当飞机在滑行时转弯时,支柱能够在某种程度上翘曲。
    • 7. 发明授权
    • Aircraft landing gear with highly offset strut pivot axis
    • 飞机起落架高度偏移支柱枢轴
    • US06805320B2
    • 2004-10-19
    • US10220526
    • 2002-08-28
    • Michel DerrienBenjamin Parzy
    • Michel DerrienBenjamin Parzy
    • B64C2510
    • B64C25/10B64C2025/345
    • An aircraft landing gear includes a leg having a strut receiving a telescopic rod to slide on a sliding axis, the strut being hinged to an aircraft structure and being capable of pivoting about a pivot axis that is highly offset from the sliding axis. The landing gear further includes a connection structure essentially comprising two panels connecting two axially separate points of the strut to a common axis structure extending along the strut pivot axis. In the gear-down position, the panels are one above the other, the top panel being connected to the strut via a high attachment which is rigid in twisting, while the bottom panel is connected to the strut via a low attachment which tolerates twisting, thereby enabling the strut to warp to some extent when the aircraft is turning while taxiing.
    • 飞机起落架包括具有支撑杆的支腿,所述支柱接收伸缩杆以在滑动轴线上滑动,所述支柱铰接到飞行器结构并且能够围绕与所述滑动轴线高度偏移的枢转轴线枢转。 起落架还包括连接结构,其基本上包括将支柱的两个轴向分离的点连接到沿着支柱枢转轴线延伸的公共轴线结构的两个面板。 在减速位置中,面板是彼此之一的,顶板通过刚性扭转的高附件连接到支柱,而底板通过低附件连接到支柱,该附件允许扭转, 从而使得当飞机在滑行时转弯时,支柱能够在某种程度上翘曲。