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    • 32. 发明授权
    • PIVOT BIN ASSEMBLY
    • EP3275785B1
    • 2018-09-12
    • 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.
    • 39. 发明公开
    • COMPACT CABIN ATTENDANT SEAT STOWAGE
    • KOMPAKTE FLUGBEGLEITERSITZVERSTAUUNG
    • EP2991899A4
    • 2017-05-10
    • EP14791218
    • 2014-04-29
    • C&D ZODIAC INC
    • NABIH NAJDREAMS EDWARDSAVIAN SCOTTZARROUATI OLIVIER
    • B64D11/06
    • B64D11/02B60N2/3018B60N2/3029B60N2/3031B60N2/3047B60N2/4855B64D11/0691
    • An aircraft monument that includes an enclosure with an enclosure interior, a compartment with a compartment interior positioned in the enclosure interior, and a stowable seat assembly disposed in the compartment. The compartment includes at least a first vertically oriented wall. The seat assembly includes a chair assembly with a back portion and a seat portion pivotably connected to the back portion along a seat pivot axis such that the seat is pivotable between closed and open positions. The chair assembly is movable between a stowed position where the seat pivot axis extends generally parallel to the first wall and the chair assembly is positioned in the compartment interior, and a deployed position where the seat pivot axis extends generally perpendicular to the first wall and the chair assembly is positioned outside of the compartment interior.
    • 一种飞机纪念碑,其包括具有外壳内部的外壳,具有定位在外壳内部中的隔室内部的隔室以及设置在隔室中的可收起座椅组件。 隔室至少包括第一竖直取向的壁。 座椅组件包括具有后部和座椅部分的座椅组件,座椅部分沿着座椅枢转轴线可枢转地连接到后部,使得座椅能够在关闭位置和打开位置之间枢转。 椅子组件可在座椅枢转轴线基本上平行于第一壁并且椅子组件被定位在舱室内部的收起位置和座椅枢转轴线大体上垂直于第一壁和第二壁的展开位置之间移动, 椅子组件定位在隔间内部的外部。
    • 40. 发明公开
    • AIRCRAFT INTERIOR BRACKET
    • FLUGZEUGINNENRAUMKLAMMER
    • EP3141766A1
    • 2017-03-15
    • EP16189539.6
    • 2014-11-13
    • C&D Zodiac, Inc.
    • TANDJUNG, DarmoSMITHSON, Tyler
    • F16B5/06F16B11/00
    • F16B5/0614F16B11/006Y10T29/49895Y10T29/49966
    • 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.
    • 组件组件包括包括要接合的表面和端面的第一部件(100)和具有限定在待接合表面中的第一形状的托架开口(30),以及至少一个支架,其包括主体 主体部分(12)具有在其间形成第一角度的第一部分(14)和第二部分(16)。 第一部分包括通过其定义的紧固件开口(18)。 第二部分包括插入件(20),并且第二部分包括至少一个通过其定义的第一粘合剂开口(22)。 所述插入部件延伸到所述支架开口中,并且所述第二部分的下表面与所述第一部件的要被接合的表面接触,其中,粘合剂将所述插入部件固定在所述托架开口内,并且其中所述第一粘合剂开口处于连通状态 支架开口。