Door for an aircraft
    11.
    发明授权

    公开(公告)号:US09981732B2

    公开(公告)日:2018-05-29

    申请号:US14900973

    申请日:2014-07-11

    Abstract: A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.

    Fastener system
    13.
    发明授权

    公开(公告)号:US09638233B1

    公开(公告)日:2017-05-02

    申请号:US15399609

    申请日:2017-01-05

    Inventor: Richard McClure

    Abstract: A fastener system that includes a female fastener assembly with a housing having a channel defined therein and a switch member movable within the channel between removing and fastening positions. The switch member includes a receiver portion having a post opening defined therein and a switch portion. The housing includes a lower opening. The post opening includes a removing portion that is aligned with the lower opening when the switch member is in the removing position and a fastening portion that is aligned with the post opening when the switch member is in the fastening position. The system also includes a male fastener assembly having a post with a slot therein. The post is received through the lower opening in the housing and the post opening so that the slot is aligned with the channel. The slot receives a portion of the receiver portion when the switch member is in the fastening position.

    Bi-fold door module
    15.
    发明授权
    Bi-fold door module 有权
    双折门模块

    公开(公告)号:US09428259B2

    公开(公告)日:2016-08-30

    申请号:US15067097

    申请日:2016-03-10

    Abstract: A door module for a vehicle lavatory that includes a bi-fold door having a first panel and a second panel each having an inner surface and an outer surface. The first and second panels are pivotably connected together by a living hinge. The living hinge includes a hinge member that extends between first and second securing members, wherein the first securing member extends along and is attached to an inner edge of the first panel and the second securing member extends along and is attached to an inner edge of the second panel.

    Abstract translation: 一种用于车辆厕所的门模块,其包括具有第一面板的双折门和分别具有内表面和外表面的第二面板。 第一和第二面板通过活动铰链可枢转地连接在一起。 活动铰链包括在第一和第二固定构件之间延伸的铰链构件,其中第一固定构件沿第一固定构件延伸并且附接到第一面板的内边缘,并且第二固定构件沿着并附接到第一面板的内边缘 第二组。

    Passenger service unit pod assembly
    16.
    发明授权
    Passenger service unit pod assembly 有权
    乘客服务单元组件

    公开(公告)号:US09365291B2

    公开(公告)日:2016-06-14

    申请号:US14612044

    申请日:2015-02-02

    Inventor: Scott Savian

    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.

    Abstract translation: 一种构造成定位在飞行器内部的个人服务单元舱组件。 个人服务单元盒组件包括个人服务单元盒和位于个人服务单元盒的正上方并被固定到其上的面板。 荚包括具有透镜组件和荚内部的壳体,位于荚内部并被配置为将灯光照射在壳体底部以下的第一阅读灯,以及位于壳体中并被配置成将光照射透镜的舱室照明 装配和住房以上。 面板包括被配置为将个人服务单元舱组件固定到飞行器内的部件的连接器。

    Aircraft interior panel with acoustic materials
    17.
    发明授权
    Aircraft interior panel with acoustic materials 有权
    飞机内部面板配有声学材料

    公开(公告)号:US09174722B2

    公开(公告)日:2015-11-03

    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。

    Pivot bin assembly
    18.
    发明授权
    Pivot bin assembly 有权
    枢轴箱组装

    公开(公告)号:US08955805B2

    公开(公告)日:2015-02-17

    申请号:US14179494

    申请日:2014-02-12

    Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

    Abstract translation: 枢轴箱组件,其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体,所述上壳体包括强力和第一和第二侧板,与所述上壳体配合以限定箱体内部的铲斗,与所述第一侧板和所述铲斗可操作地相关联的第一枢转机构,以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一和第二枢转机构沿着枢转轴线轴向对齐,使得该斗围绕上部壳体的枢转轴线在打开位置和关闭位置之间枢转。

    PIVOT BIN ASSEMBLY
    19.
    发明申请
    PIVOT BIN ASSEMBLY 有权
    PIVOT BIN装配

    公开(公告)号:US20140197721A1

    公开(公告)日:2014-07-17

    申请号:US14179494

    申请日:2014-02-12

    Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

    Abstract translation: 枢轴箱组件,其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体,所述上壳体包括强背和第一和第二侧板,与所述上壳体协作以限定仓室内部的桶,与所述第一侧板和所述桶可操作地相关联的第一枢转机构,以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一和第二枢转机构沿着枢转轴线轴向对齐,使得该斗围绕枢转轴线相对于上壳体在打开位置和关闭位置之间枢转。

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