AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS
    121.
    发明申请
    AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS 有权
    具有声学材料的飞机内部面板

    公开(公告)号:US20150144734A1

    公开(公告)日:2015-05-28

    申请号:US14589906

    申请日:2015-01-05

    CPC classification number: B64C1/40 B64C1/066

    Abstract: A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed therein that extend inwardly. The rib members include an inner surface and an outer surface. A plurality of panel portions are defined between the plurality of rib members. The panel portions include an inner surface and an outer surface. The inner surface of the rib members are secured to the inner surface of the first panel, and the inner surface of the panel portions is spaced apart from the inner surface of the first panel to define at least first and second cavities.

    Abstract translation: 一种面板组件,其包括具有内表面和外表面的第一面板,以及具有内表面和外表面的第二面板。 第二面板包括在其中形成的多个向内延伸的肋构件。 肋构件包括内表面和外表面。 在多个肋构件之间限定多个面板部。 面板部分包括内表面和外表面。 肋构件的内表面固定到第一面板的内表面,并且面板部分的内表面与第一面板的内表面间隔开以限定至少第一和第二空腔。

    AIRCRAFT INTERIOR BRACKET
    122.
    发明申请
    AIRCRAFT INTERIOR BRACKET 有权
    飞机内部支架

    公开(公告)号:US20150129728A1

    公开(公告)日:2015-05-14

    申请号:US14540195

    申请日:2014-11-13

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

    Abstract: A bracket that includes a main body portion having a first portion and a second portion that form a first angle therebetween. The first portion includes opposing front and rear surfaces and the second portion includes opposing upper and lower surfaces. The first portion includes a fastener opening defined therethrough, the second portion includes an insert feature extending from the lower surface, and the second portion includes at least one adhesive opening defined therethrough.

    Abstract translation: 一种支架,其包括具有第一部分的主体部分和在它们之间形成第一角度的第二部分。 第一部分包括相对的前表面和后表面,并且第二部分包括相对的上表面和下表面。 第一部分包括限定在其中的紧固件开口,第二部分包括从下表面延伸的插入件,并且第二部分包括至少一个通过其限定的粘合剂开口。

    LAVATORY MONUMENT WITH STORAGE COMPARTMENT
    123.
    发明申请
    LAVATORY MONUMENT WITH STORAGE COMPARTMENT 审中-公开
    带储物柜的洗衣机

    公开(公告)号:US20140291446A1

    公开(公告)日:2014-10-02

    申请号:US14304262

    申请日:2014-06-13

    CPC classification number: B64D11/02

    Abstract: A lavatory monument assembly configured to be positioned in the interior of a vehicle. The lavatory monument assembly includes an enclosure that defines a first lavatory interior and includes at least a front wall and first and second side walls extending rearwardly from the front wall. The first lavatory interior includes a urinal positioned therein. The lavatory monument assembly also includes a first storage compartment positioned in the first lavatory interior. The first storage compartment includes a first storage door that is movable between an open position and a closed position. The front wall includes a first lavatory door that is movable between a closed and an open position and provides access to the first lavatory interior.

    Abstract translation: 构造成定位在车辆内部的盥洗室纪念碑组件。 盥洗室纪念碑组件包括限定第一盥洗室内部并且至少包括前壁以及从前壁向后延伸的第一和第二侧壁的外壳。 第一盥洗室内部包括定位在其中的小便池。 卫生间纪念碑装置还包括位于第一洗手间内部的第一储藏室。 第一储藏室包括可在打开位置和关闭位置之间移动的第一储存门。 前壁包括可在闭合位置和打开位置之间移动的第一盥洗室门,并提供通向第一盥洗室内部的通道。

    READING LIGHT
    124.
    发明申请
    READING LIGHT 审中-公开
    阅读灯

    公开(公告)号:US20140192544A1

    公开(公告)日:2014-07-10

    申请号:US14150603

    申请日:2014-01-08

    CPC classification number: F21V15/012 B64D11/00 B64D47/02 B64D2011/0053

    Abstract: A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions.

    Abstract translation: 一种照明组件,其包括限定外部壳体轴线的外部壳体,限定内部壳体轴线的内部壳体和定位在所述内部壳体中的轻型构件。 外壳包括具有前开口的前表面和限定具有截头球形的调节空腔的内表面。 内壳体具有截头球形并且至少部分地容纳在调节空腔内。 内壳体在其中限定一个光凹槽,并且包括其中限定有孔的前盖。 前盖至少部分地限定光凹部。 光构件限定光轴。 光轴和内壳体轴线不是同轴的并且不平行并且在它们之间形成一个角度。 内壳体在原位置和多个调节位置之间是可调节的。

    GRAPHICS DISPLAY MODULE
    125.
    发明申请
    GRAPHICS DISPLAY MODULE 有权
    图形显示模块

    公开(公告)号:US20140160775A1

    公开(公告)日:2014-06-12

    申请号:US14102486

    申请日:2013-12-10

    CPC classification number: F21V21/00 B64D45/00 B64D2045/007 F21S45/00

    Abstract: A graphics display module that includes a frame with a front portion and a rear portion that cooperate to secure a hated panel having a front surface and a rear surface therebetween. The front portion defines a central opening through which the front surface of the lighted panel can be viewed, The front portion and rear portion cooperate to define a channel that includes lighting disposed therein that is configured to back light the lighted panel.

    Abstract translation: 图形显示模块,其包括具有前部和后部的框架,所述框架协作以固定具有前表面和后表面的讨厌面板。 前部分限定中心开口,照明面板的前表面可通过该中心开口被观看。前部分和后部协作以形成包括设置在其中的照明通道的通道,该通道被配置为背光点亮点亮的面板。

    AIRCRAFT AISLE PARTITION WITH SWINGING DOORS
    126.
    发明申请
    AIRCRAFT AISLE PARTITION WITH SWINGING DOORS 有权
    飞机离合器与开关门

    公开(公告)号:US20140158826A1

    公开(公告)日:2014-06-12

    申请号:US14102473

    申请日:2013-12-10

    CPC classification number: B64D11/0023 B64D11/02 B64D11/04

    Abstract: A partition configured to be positioned within an aircraft. The partition includes a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member. The first jamb member includes first lighting that illuminates the first door, and the first door is movable between a stowed position and a deployed position. The partition also includes a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member. The second jamb member includes second lighting that illuminates the second door, and the second door is movable between a stowed position and a deployed position. The second door is spaced apart from the first door.

    Abstract translation: 配置成定位在飞行器内的分隔件。 隔板包括第一分隔件组件,该第一分隔组件包括第一壁部分,第一壁部分具有固定到其内侧表面的第一侧柱部件和铰接地连接到第一侧柱部件的第一门。 第一侧柱构件包括照亮第一门的第一照明,并且第一门可在收起位置和展开位置之间移动。 分隔件还包括第二分隔件组件,其包括具有固定到其内侧表面的第二侧柱构件的第二壁部分和铰接地连接到第二侧柱构件的第二门。 第二侧柱构件包括照亮第二门的第二照明,并且第二门可在收起位置和展开位置之间移动。 第二扇门与第一扇门隔开。

    PSU POD ASSEMBLY AND METHOD FOR USING SAME
    127.
    发明申请
    PSU POD ASSEMBLY AND METHOD FOR USING SAME 有权
    PSU POD组装及其使用方法

    公开(公告)号:US20130208490A1

    公开(公告)日:2013-08-15

    申请号:US13765646

    申请日:2013-02-12

    Inventor: Scott Savian

    Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.

    Abstract translation: 被配置为定位在飞行器内部的PSU舱组件。 PSU盒组件包括PSU盒,其包括壳体,壳体包括顶部,底部以及第一,第二,第三和第四侧,其协作以限定荚内部和位于PSU荚上方并连接到PSU荚的面板。 PSU舱包括至少位于舱内部的第一和第二读取灯,其被配置成将光照射在壳体下方,并且定位在壳体上或壳体中的舱灯,该灯被配置为在壳体上方照射光。 该面板包括被配置为将PSU盒组件固定到飞行器内的组件的连接器。

    Pivot bin with lift assist assembly and method of use thereof

    公开(公告)号:US10907392B2

    公开(公告)日:2021-02-02

    申请号:US15878210

    申请日:2018-01-23

    Abstract: A method of pivoting an aircraft storage bin that includes a bucket that pivots with respect to an upper housing. The method includes pivoting the bucket from a closed position to an intermediate position and placing weight that exceeds a predetermined weight threshold in the bucket, thereby causing the bucket to move to an open position. Movement of the bucket to the open position causes a lift assist unit to activate. A first end of the lift assist unit is connected to the bucket and a second end of the lift assist unit is connected to the upper housing. The method also includes pivoting the bucket from the open position to the closed position. The lift assist unit provides assistance as the bucket is pivoting from the open position to the closed position.

    DUAL URINAL LAVATORY MONUMENT
    129.
    发明申请

    公开(公告)号:US20200223549A1

    公开(公告)日:2020-07-16

    申请号:US16833465

    申请日:2020-03-27

    Abstract: A lavatory monument configured to be positioned in an aircraft interior that includes an enclosure that includes first, second, third and fourth walls, and defines a lavatory interior, a first lavatory compartment that includes a first urinal unit positioned therein, and a second lavatory compartment that includes a second urinal unit positioned therein. The first lavatory compartment includes a first door and the second lavatory compartment includes a second door. A divider wall separates at least a portion of the first lavatory compartment from at least a portion of the second lavatory compartment. The first door is positioned on one of the first or second walls and the second door is positioned on one of the first or third walls.

    Baggage management system
    130.
    发明授权

    公开(公告)号:US10713617B2

    公开(公告)日:2020-07-14

    申请号:US16024448

    申请日:2018-06-29

    Abstract: A baggage management system for a vehicle that includes a storage bin that defines a bin interior, a baggage monitoring system associated with the storage bin, and a display member associated with the storage bin. The baggage monitoring system is configured to monitor the positioning of baggage within the bin interior and the display member is configured to provide baggage positioning information to passengers.

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