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    • 122. 发明申请
    • INSTALLATION SYSTEM FOR AFT AIRCRAFT MONUMENT ASSEMBLY
    • AFT飞机纪念大会安装系统
    • WO2016070118A1
    • 2016-05-06
    • PCT/US2015/058450
    • 2015-10-30
    • C&D ZODIAC, INC.
    • NAJD, NabihTA, Harry
    • B64D11/00
    • B64D11/00B64D11/02B64D11/04B64D2011/0046B64F5/10Y10T29/49826Y10T29/49904Y10T29/49947Y10T29/49948Y10T29/49963
    • A method of positioning a monument within an aircraft. The method includes positioning first and second tracks having first and second carriages thereon on the floor. The first and second carriages are initially in a first position. The method includes positioning a floor of a first monument section with a first fitting on the carriage of the first track, positioning a floor of a second monument section with a second fitting on the carriage of the second track, moving the first and second monument sections with the carriages to a second position, aligning the first fittings with a connection point on the aircraft floor, raising the floors of the first and second monument sections and removing the first and second tracks, lowering the floors of the first and second monument sections, securing the first and second fittings to the connection points associated therewith.
    • 在飞机内定位纪念碑的方法。 该方法包括将第一和第二轨道的第一和第二轨道定位在地板上。 第一和第二支架最初处于第一位置。 该方法包括将具有第一配件的第一纪念碑部分的地板定位在第一轨道的托架上,将具有第二配件的第二纪念碑部分的地板定位在第二轨道的托架上,使第一和第二纪念碑部分移动 将所述托架移动到第二位置,使所述第一配件与所述飞机地板上的连接点对准,升高所述第一和第二纪念碑部分的地板并且移除所述第一和第二轨道,降低所述第一和第二纪念碑部分的地板, 将第一和第二配件固定到与其相关联的连接点。
    • 123. 发明申请
    • LAVATORY MONUMENT WITH STORAGE COMPARTMENT
    • 带储物柜的洗衣机
    • WO2014201397A1
    • 2014-12-18
    • PCT/US2014/042367
    • 2014-06-13
    • C&D ZODIAC, INC.
    • REAMS, EdwardSWAIN, GlennSCOLEY, Ian GeoffreyNAJD, Nabih
    • B64D11/02
    • B64D11/02
    • 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.
    • 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。
    • 126. 发明申请
    • PIVOT BIN ASSEMBLY
    • PIVOT BIN总成
    • WO2013123070A1
    • 2013-08-22
    • PCT/US2013/025962
    • 2013-02-13
    • C&D ZODIAC, INC.
    • SAVIAN, ScottKEARSEY, Stephen
    • B64D11/00
    • B64D13/00B60Q3/225B60Q3/43B64D11/0015B64D11/003B64D2011/0038Y02T50/46Y10T29/49002
    • 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.
    • 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 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。
    • 127. 发明申请
    • ROTARY DAMPING MECHANISM WITH PIVOTAL VANES
    • 旋转阻尼机构与双向风扇
    • WO2013123069A1
    • 2013-08-22
    • PCT/US2013/025961
    • 2013-02-13
    • C&D ZODIAC, INC.
    • KEARSEY, StephenMCCLURE, Richard
    • E05F5/00
    • F01D25/04E05D7/081E05D7/083E05F3/14E05F3/20E05Y2201/21E05Y2201/234E05Y2900/502E05Y2900/538
    • 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.
    • 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。
    • 129. 发明申请
    • FREEWHEELING ROTARY DAMPING MECHANISM
    • 自由旋转阻尼机构
    • WO2013123054A1
    • 2013-08-22
    • PCT/US2013/025945
    • 2013-02-13
    • C&D ZODIAC, INC.
    • KEARSEY, StephenMCCLURE, Richard
    • F16F9/12
    • F16F9/3207A47B46/00B64D11/003F16F9/145
    • 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.
    • 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。