STORAGE BIN WITH LUGGAGE POSITIONING PROTRUSIONS

    公开(公告)号:EP3386860A1

    公开(公告)日:2018-10-17

    申请号:EP16873574.4

    申请日:2016-11-18

    CPC classification number: B64D11/003

    Abstract: An aircraft storage bin that includes an upper housing and a bucket movable with respect to the upper housing between a closed position and an open position. The upper housing and the bucket cooperate to define a bin interior. The bucket includes a bottom and first and second opposing side walls. The bottom of the bucket includes an outer surface, an inner surface, a front edge, and first and second protrusions protruding into the bin interior. The first protrusion defines a first luggage engaging surface and the second protrusion defines a second luggage engaging surface. The first protrusion includes an inner surface and an outer surface that defines a channel. The channel includes at least a portion of a latch button assembly disposed therein. The first and second cables extend outwardly from the latch button assembly and through the channel. The bucket includes a cover further partially defining the channel.

    PIVOT BIN ASSEMBLY
    32.
    发明授权

    公开(公告)号:EP3275785B1

    公开(公告)日:2018-09-12

    申请号:EP17184027.5

    申请日:2014-02-13

    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.

    TOILET MODULE
    33.
    发明公开
    TOILET MODULE 审中-公开

    公开(公告)号:EP3355754A1

    公开(公告)日:2018-08-08

    申请号:EP16852215.9

    申请日:2016-03-30

    CPC classification number: B64D11/02 E03D11/14

    Abstract: A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall. The retainer member includes a wall attachment flange and a press fit portion extending generally inwardly from the wall attachment flange. When the retainer member is secured to a wall a channel is defined between the wall and the press fit portion. The attachment assembly also includes a seal member that includes a bulge portion that is received in the channel of the retainer member.

    PASSENGER SERVICE UNIT POD ASSEMBLY
    34.
    发明公开
    PASSENGER SERVICE UNIT POD ASSEMBLY 审中-公开
    乘客服务单位POD组件

    公开(公告)号:EP3253622A1

    公开(公告)日:2017-12-13

    申请号:EP15881361.8

    申请日:2015-02-05

    Inventor: SAVIAN, Scott

    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.

    CEILING PANEL ASSEMBLY AND MOUNTING SYSTEM THEREFOR
    36.
    发明公开
    CEILING PANEL ASSEMBLY AND MOUNTING SYSTEM THEREFOR 审中-公开
    天花板组装及安装系统

    公开(公告)号:EP3250457A1

    公开(公告)日:2017-12-06

    申请号:EP16744223.5

    申请日:2016-01-29

    Abstract: A module for mounting within a ceiling panel assembly. The module includes an upper mounting frame that includes a main body portion that defines a central opening, a lower mounting frame that is at least partially received in the central opening of the upper mounting frame, and a latch assembly. The main body portion of the upper mounting frame includes a flange extending outwardly therefrom. The lower mounting frame is pivotable with respect to the upper mounting frame between a first position and a second position. The latch assembly is associated with a first end of the upper mounting frame and the lower mounting frame. When the latch assembly is released the lower mounting frame pivots from the first position to the second position.

    AIRCRAFT INTERIOR BRACKET
    37.
    发明公开

    公开(公告)号:EP3068689A4

    公开(公告)日:2017-11-01

    申请号:EP14861422

    申请日:2014-11-13

    Applicant: C&D ZODIAC INC

    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.

    OVERHEAD STORAGE BIN LATCH SYSTEM
    38.
    发明公开
    OVERHEAD STORAGE BIN LATCH SYSTEM 审中-公开
    顶置存储卡锁系统

    公开(公告)号:EP3212501A1

    公开(公告)日:2017-09-06

    申请号:EP15855175.4

    申请日:2015-10-27

    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.

    Abstract translation: 本发明涉及一种闩锁系统,该闩锁系统包括具有可在初始位置和致动位置之间移动的按钮的拨片按钮组件,包括第一撞针组件和第一挂钩组件的第一闩锁组件以及在桨按钮 组件和第一闩锁组件。 按钮从原始位置到致动位置的移动移动第一缆线,从而使第一钩组件和第一撞针组件脱离接合。

    COMPACT CABIN ATTENDANT SEAT STOWAGE
    39.
    发明公开
    COMPACT CABIN ATTENDANT SEAT STOWAGE 有权
    KOMPAKTE FLUGBEGLEITERSITZVERSTAUUNG

    公开(公告)号:EP2991899A4

    公开(公告)日:2017-05-10

    申请号:EP14791218

    申请日:2014-04-29

    Applicant: C&D ZODIAC INC

    Abstract: 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.

    Abstract translation: 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。

    AIRCRAFT INTERIOR BRACKET
    40.
    发明公开
    AIRCRAFT INTERIOR BRACKET 有权
    FLUGZEUGINNENRAUMKLAMMER

    公开(公告)号:EP3141766A1

    公开(公告)日:2017-03-15

    申请号:EP16189539.6

    申请日:2014-11-13

    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.

    Abstract translation: 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。

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