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    • 41. 发明申请
    • CEILING PANEL ASSEMBLY AND MOUNTING SYSTEM THEREFOR
    • 天花板组件及其安装系统
    • US20160222654A1
    • 2016-08-04
    • US15011215
    • 2016-01-29
    • C&D ZODIAC, INC.
    • Bruce ShimizuScott Savian
    • E04B9/00B64D11/02B64C1/06F16M13/02
    • E04B9/006B64C1/066B64D11/02E04B9/003
    • 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.
    • 用于安装在天花板面板组件内的模块。 模块包括上部安装框架,其包括限定中心开口的主体部分,至少部分地容纳在上部安装框架的中心开口中的下部安装框架和闩锁组件。 上安装框架的主体部分包括从其向外延伸的凸缘。 下安装框架可相对于上安装框架在第一位置和第二位置之间枢转。 闩锁组件与上安装框架和下安装框架的第一端相关联。 当闩锁组件被释放时,下安装框架从第一位置枢转到第二位置。
    • 44. 发明申请
    • PIVOT BIN ASSEMBLY
    • PIVOT BIN总成
    • US20150151839A1
    • 2015-06-04
    • US14622377
    • 2015-02-13
    • C&D ZODIAC, INC.
    • Scott SavianCorey Williams
    • B64D11/00
    • B64D11/003B60Q3/43B64D11/0015B64D2011/0038Y02T50/46
    • 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.
    • 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。
    • 45. 发明授权
    • Lavatory Monument Assembly
    • 洗手间纪念碑大会
    • US09045230B2
    • 2015-06-02
    • US13765612
    • 2013-02-12
    • C&D ZODIAC, INC.
    • Ralph BurrowsChristoph GoeschelJohn HigginsThomas LeeHerman SchotteScott SavianIan G. Scoley
    • B64D11/02
    • B64D11/02B64D11/0691
    • A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes a first wall and a second wall that are generally parallel to one another, and the second wall is longer than the first wall. The lavatory monument assembly further includes a third wall and a fourth wall, and the third wall and the fourth wall generally are perpendicular to the first wall and the second wall, and the third wall and the fourth wall connect to the first wall and the second wall to form a lavatory interior. The first portion of the fourth wall generally is parallel to the third wall, and a second portion of the fourth wall angles inwardly along generally straight lines into the lavatory interior, such that the area in the lavatory interior proximate the first wall is less than the area proximate the second wall. The lavatory monument assembly farther includes a toilet in the lavatory interior proximate the first wall, and it further includes a door positioned on one of the first, second, third, or fourth walls.
    • 一种构造成定位在飞行器内部的卫生间纪念碑组件,其包括大致彼此平行的第一壁和第二壁,并且第二壁比第一壁长。 卫生间纪念碑组件还包括第三壁和第四壁,第三壁和第四壁通常垂直于第一壁和第二壁,第三壁和第四壁连接到第一壁,第二壁连接到第一壁 墙壁形成盥洗室内部。 第四壁的第一部分通常平行于第三壁,并且第四壁的第二部分沿大致直线向内倾斜进入盥洗室内部,使得靠近第一壁的盥洗室内部的区域小于 靠近第二个墙的区域。 卫生间纪念碑组件还包括靠近第一墙壁的盥洗室内部的卫生间,并且还包括位于第一,第二,第三或第四壁之一上的门。
    • 46. 发明申请
    • DESIGN OPTIMIZER SYSTEM
    • 设计优化系统
    • US20140278270A1
    • 2014-09-18
    • US13841840
    • 2013-03-15
    • C&D ZODIAC, INC.
    • Scott SavianSandesh ShettyAdam Sbeglia
    • G06F17/50
    • G06F17/5095B64D11/00B64D11/06G06F2217/02G06F2217/46
    • A computerized system for optimizing the design layout of an aircraft configured to execute, by at least one processor, the instructions of one or more software modules stored on a nonvolatile computer readable medium, the system comprising a first software module configured to receive input from a user regarding number of seats; a second software module configured to receive input from a user regarding seat pitch; a third software module configured to receive input from a user regarding meal service; a fourth software module configured to receive input from a user regarding beverage service; a fifth software module configured to comprise a listing of all possible combinations of all aircraft interior layout configurations for an aircraft. The sixth software module uses the inputs from one or more of the first, second, third, or fourth software modules to determine and create an output of the one configuration that takes up the least amount of seat space, weighs the least, and contains the most amount of aircraft cabin storage space. A seventh software module graphically displays the output of the sixth software module.
    • 一种用于优化被配置为由至少一个处理器执行存储在非易失性计算机可读介质上的一个或多个软件模块的指令的飞行器的设计布局的计算机化系统,所述系统包括第一软件模块,所述第一软件模块被配置为从 用户关于座位数; 第二软件模块,被配置为从用户接收关于座椅音高的输入; 第三软件模块,被配置为从用户接收关于膳食服务的输入; 第四软件模块,被配置为从用户接收关于饮料服务的输入; 第五软件模块被配置为包括用于飞行器的所有飞行器内部布局配置的所有可能组合的列表。 第六软件模块使用来自第一,第二,第三或第四软件模块中的一个或多个的输入来确定和创建占据最少座位空间的一个配置的输出,至少重量,并且包含 大多数飞机机舱的存储空间。 第七个软件模块以图形方式显示第六个软件模块的输出。