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    • 64. 发明公开
    • DESIGN OPTIMIZER SYSTEM
    • 设计优化器系统
    • EP2969754A1
    • 2016-01-20
    • EP13877481.5
    • 2013-05-28
    • C&D Zodiac, Inc.
    • SAVIAN, ScottSHETTY, SandeshSBEGLIA, Adam
    • B64D11/06
    • 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.
    • 一种用于优化飞机的设计布局的计算机化系统,所述飞机的设计布局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,所述系统包括第一软件模块,所述第一软件模块被配置为接收来自 用户关于座位数量; 第二软件模块,其被配置为从用户接收关于座位间距的输入; 第三软件模块,其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,其被配置为包括航空器的所有飞机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并创建占用最少量座位空间的一个配置的输出,其重量最小并包含 最多的飞机机舱存储空间。 第七个软件模块以图形方式显示第六个软件模块的输出。
    • 68. 发明公开
    • PIVOT BIN ASSEMBLY
    • EP2814737A1
    • 2014-12-24
    • EP13749848.1
    • 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.
    • 枢转仓组件被配置为接收行李并被定位在飞机的内部。 枢转仓组件包括:上部壳体,其包括强力背板以及第一和第二侧板;与上部壳体协作以限定仓内部的铲斗;与第一侧板和铲斗可操作地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枢转轴线轴向对齐并且可围绕枢转轴线旋转,使得桶在打开位置与关闭位置之间围绕枢转轴线相对于上部壳体枢转。