Freewheeling rotary damping mechanism
    2.
    发明授权
    Freewheeling rotary damping mechanism 有权
    续流旋转阻尼机构

    公开(公告)号:US08899390B2

    公开(公告)日:2014-12-02

    申请号:US13765358

    申请日:2013-02-12

    CPC classification number: F16F9/3207 A47B46/00 B64D11/003 F16F9/145

    Abstract: A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein. When the axle shaft rotates in the first direction, the transmission assembly transmits rotation from the axle shaft to the vane, and when the axle shaft rotates in the second direction, the transmission assembly transmits less rotation to the first vane than when the axle shaft rotates in the first direction.

    Abstract translation: 一种阻尼机构,包括具有由组件外座圈限定的内圆周表面的壳体,可相对于所述壳体旋转的车轴,以及与所述车轴一起操作地配置并设置在所述壳体内的变速器组件。 传动组件包括组合中间座圈。 在组件中间座圈和组件外圈的内圆周表面之间限定包括流体的流体空间。 叶片设置在组装中间座圈和组件外圈的内周面之间。 叶片包括其中限定的限制空间。 当车轴沿第一方向旋转时,传动组件将转轴从轴轴传递到叶片,并且当车轴沿第二方向旋转时,传动组件相对于第一叶片的旋转少于当车轴旋转时 在第一个方向。

    Pivot bin assembly
    4.
    发明授权
    Pivot bin assembly 有权
    枢轴箱组装

    公开(公告)号:US09162617B2

    公开(公告)日:2015-10-20

    申请号:US13765652

    申请日:2013-02-12

    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 and are rotatable about 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。 第一枢转机构和第二枢转机构沿着枢轴对准并且可以围绕枢转轴线旋转,使得所述挖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。

    Overhead storage bin latch system

    公开(公告)号:US10647430B2

    公开(公告)日:2020-05-12

    申请号:US15674342

    申请日:2017-08-10

    Abstract: A latch system that includes a paddle button assembly having a button that is movable between home and actuation positions, a latch assembly that includes a striker assembly with a striker and a hook assembly, and a cable that extends between the paddle button and latch assembly. The hook assembly includes a hook, a pivotal trigger arm, and a manual override switch that is movable between first and second positions when the trigger arm is moved from an engaged position to a disengaged position. Movement of the button from the home position to the actuation position pushes or pulls the cable, thereby pivoting the trigger arm from the engaged to the disengaged position and disengaging the hook from the striker. Pivotal movement of the trigger arm from the engaged to the disengaged position results in linear movement of the manual override switch from the first to the second position.

    ROTARY DAMPING MECHANISM WITH PIVOTAL VANES
    7.
    发明申请
    ROTARY DAMPING MECHANISM WITH PIVOTAL VANES 审中-公开
    旋转阻尼机构与双向风扇

    公开(公告)号:US20130209221A1

    公开(公告)日:2013-08-15

    申请号:US13765435

    申请日:2013-02-12

    Abstract: A damping mechanism that includes a housing having fluid disposed therein and an inner circumferential surface, an axle shaft that is rotatable with respect to the housing, and a first vane having a distal end and being pivotally associated with the axle shaft. When the axle shaft rotates in a first direction, the first vane pivots to a deployed position, and when the axle shaft rotates in a second direction, the first vane pivots to a stowed position. A first clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the deployed position, and a second clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the stowed position. The second clearance is greater than the first clearance.

    Abstract translation: 一种阻尼机构,其包括具有设置在其中的流体和内周面的壳体,能够相对于所述壳体旋转的车轴,以及具有远端并与所述车轴枢转连接的第一叶片。 当车轴沿第一方向旋转时,第一叶片枢转到展开位置,并且当车轴沿第二方向旋转时,第一叶片枢转到收起位置。 当第一叶片处于展开位置时,在第一叶片的远端和壳体的内周面之间限定第一间隙,并且在第一叶片的远端和内周面之间限定第二间隙 的第一个叶片处于收起位置。 第二间隙大于第一间隙。

    PIVOT BIN ASSEMBLY
    8.
    发明申请
    PIVOT BIN ASSEMBLY 有权
    PIVOT BIN总成

    公开(公告)号:US20130206903A1

    公开(公告)日:2013-08-15

    申请号:US13765652

    申请日:2013-02-12

    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 and are rotatable about 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 与第二侧板和铲斗可操作地相关联的第二枢转机构。 第一枢转机构和第二枢转机构沿着枢轴对准并且可以围绕枢转轴线旋转,使得所述挖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。

    AIRCRAFT WITH PARTITION SYSTEM
    9.
    发明申请

    公开(公告)号:US20200180766A1

    公开(公告)日:2020-06-11

    申请号:US16790535

    申请日:2020-02-13

    Abstract: An aircraft partition system that includes a first partition assembly that includes a carriage assembly that is configured to be secured to at least one of first and second passenger service unit rails and a divider wall having first and second opposing sides and extending downwardly from the carriage assembly.

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