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    PASSENGER SERVICE UNIT POD ASSEMBLY
    105.
    发明公开
    PASSENGER SERVICE UNIT POD ASSEMBLY 审中-公开

    公开(公告)号：EP3253622A4

    公开(公告)日：2018-07-04

    申请号：EP15881361

    申请日：2015-02-05

    Applicant: C&D ZODIAC INC

    Inventor： SAVIAN SCOTT

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  B64D11/00 ,  B64D2011/0038 ,  B64D2011/0053 ,  B64D2013/003 ,  Y02T50/46

    Abstract: A personal service unit pod assembly configured to be positioned in the interior of an aircraft. The personal service unit pod assembly includes a personal service unit pod and a panel positioned directly above and affixed to the personal service unit pod. The pod includes a housing with a lens assembly and a pod interior, a first reading light positioned within the pod interior and configured to shine light below the bottom of the housing, and cabin lighting positioned in the housing and configured to shine light through the lens assembly and above the housing. The panel includes connectors that are configured to secure the personal service unit pod assembly to a component within the aircraft.

    OVERHEAD STORAGE BIN LATCH SYSTEM
    106.
    发明公开
    OVERHEAD STORAGE BIN LATCH SYSTEM 审中-公开

    公开(公告)号：EP3212501A4

    公开(公告)日：2018-06-06

    申请号：EP15855175

    申请日：2015-10-27

    Applicant: C&D ZODIAC INC

    Inventor： KEARSEY STEPHEN ,  LONG ERIC ,  SAVIAN SCOTT

    IPC: B64D11/00 ,  E05B53/00

    CPC classification number: B64D11/003 ,  E05B41/00 ,  E05B53/005 ,  E05C3/24 ,  E05C9/00

    Abstract: A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly, and a first cable that extends between the paddle button assembly and the first latch assembly. Movement of the button from the home position to the actuation position moves the first cable, thereby disengaging the first hook assembly and the first striker assembly.

    AIRCRAFT INTERIOR BRACKET
    107.
    发明授权
    AIRCRAFT INTERIOR BRACKET 有权
    飞机内部支架

    公开(公告)号：EP3141766B1

    公开(公告)日：2018-03-28

    申请号：EP16189539.6

    申请日：2014-11-13

    Applicant: C&D Zodiac, Inc.

    Inventor： TANDJUNG, Darmo ,  SMITHSON, Tyler

    IPC: F16B5/06 ,  F16B11/00

    CPC classification number: F16B5/0614 ,  F16B11/006 ,  Y10T29/49895 ,  Y10T29/49966

    Abstract: A component assembly comprises a first component (100) that includes a surface to be joined and an end surface, and a bracket opening (30) having a first shape defined in the surface to be joined, and at least one bracket that includes a main body portion (12) having a first portion (14) and a second portion (16) that form a first angle therebetween. The first portion includes a fastener opening (18) defined therethrough. The second portion includes an insert feature (20), and the second portion includes at least a first adhesive opening (22) defined therethrough. The insert feature extends into the bracket opening and the lower surface of the second portion is in contact with the surface to be joined of the first component, wherein an adhesive secures the insert feature within the bracket opening and wherein the first adhesive opening is in communication with the bracket opening.

    PIVOT BIN ASSEMBLY
    108.
    发明公开
    PIVOT BIN ASSEMBLY 有权

    公开(公告)号：EP3275785A1

    公开(公告)日：2018-01-31

    申请号：EP17184027.5

    申请日：2014-02-13

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott ,  KEARSEY, Stephen ,  WILLIAMS, Corey

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  B64D2011/0038 ,  B64D2011/0053 ,  Y02T50/46

    Abstract: 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.

    Abstract translation: 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。

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