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    • 14. 发明公开
    • PIVOT BIN ASSEMBLY
    • EP3275785A1
    • 2018-01-31
    • EP17184027.5
    • 2014-02-13
    • C&D Zodiac, Inc.
    • SAVIAN, ScottKEARSEY, StephenWILLIAMS, Corey
    • B64D11/00
    • B64D11/003B64D2011/0038B64D2011/0053Y02T50/46
    • There is provided a pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly comprises: an upper housing that includes a strongback and first and second side panels which include a bottom edge; a bucket that cooperates with the upper housing to define a bin interior, wherein the bucket includes a bottom and first and second opposing sides which include a top edge, and wherein, when the pivot bin assembly receives luggage in the bin interior, the luggage is positioned on the bottom of the bucket, which bears the load of the luggage; a first pivot mechanism operatively associated with the first side panel and the bucket; a second pivot mechanism operatively associated with the second side panel and the bucket, such that the bucket pivots with respect to the upper housing between an open position and a closed position, wherein, in the closed position, at least a portion of the top edge of the first side of the bucket abuts the bottom edge of the first side panel, and at least a portion of the top edge of the second side of the bucket abuts the bottom edge of the second side panel; a first connecting unit having a first end pivotally connected to the first side of the bucket and a second end pivotally connected to the first side panel; and a second connecting unit having a first end pivotally connected to the second side of the bucket and a second end pivotally connected to the second side panel, wherein the first and second connecting units provide one or both of damping when the bucket pivots to the open position and/or assistance when the bucket pivots to the closed position.
    • 提供了一种枢轴仓组件,其被配置为接收行李并被定位在飞机的内部。 所述枢转仓组件包括:上部壳体,其包括强力背板以及包括底部边缘的第一和第二侧板; 所述桶与所述上部壳体协作以限定箱内部,其中所述箱包括底部以及包括顶部边缘的第一和第二相对侧,并且其中当所述枢转仓组件接收到仓内的行李时,所述行李箱 位于桶的底部,承载行李的重量; 第一枢转机构,其可操作地与所述第一侧板和所述桶相关联; 第二枢转机构,所述第二枢转机构与所述第二侧板和所述铲斗可操作地相关联,使得所述铲斗相对于所述上部壳体在打开位置和关闭位置之间枢转,其中,在所述关闭位置,所述顶部边缘的至少一部分 所述铲斗的所述第一侧的顶边的至少一部分邻接所述第一侧板的所述底边;以及所述铲斗的所述第一侧的所述顶边的至少一部分邻接所述第一侧板的所述底边。 第一连接单元,其具有枢转地连接到所述桶的所述第一侧的第一端和枢转地连接到所述第一侧板的第二端; 以及第二连接单元,所述第二连接单元具有枢转地连接至所述铲斗的所述第二侧的第一端和枢转地连接至所述第二侧板的第二端,其中,所述第一连接单元和所述第二连接单元提供所述铲斗枢转至所述开口 位置和/或当铲斗枢转到关闭位置时的辅助。
    • 17. 发明公开
    • PIVOT BIN ASSEMBLY
    • EP3166847A1
    • 2017-05-17
    • EP15818886.2
    • 2015-07-10
    • C&D Zodiac, Inc.
    • SAVIAN, Scott
    • B64D11/00
    • B64D11/003Y02T50/46
    • An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge and first and second opposing side walls extending upwardly from the bottom and pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance.
    • 一种飞机储物箱,其包括上部壳体和枢转地连接到上部壳体的铲斗,该上部壳体与上部壳体协作以限定箱内部。 该桶包括底部,前边缘以及从底部向上延伸的第一和第二相对侧壁,并且在打开位置和关闭位置之间围绕枢转轴线相对于上部壳体枢转。 当储存箱安装在飞机中时,第一水平距离限定在当铲斗处于关闭位置时延伸穿过枢转轴线的第一竖直线与铲斗的前边缘之间,并且限定第二水平距离 当铲斗处于打开位置时,在第一竖直线与铲斗的前边缘之间。 第一水平距离大于第二水平距离。