会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 11. 发明申请
    • PIVOT BIN ASSEMBLY
    • PIVOT BIN总成
    • WO2014127161A1
    • 2014-08-21
    • PCT/US2014/016313
    • 2014-02-13
    • C&D ZODIAC, INC.
    • SAVIAN, ScottKEARSEY, StephenWILLIAMS, Corey
    • B64D11/00
    • B64D11/003B64D2011/0038B64D2011/0053Y02T50/46
    • 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。
    • 16. 发明申请
    • SHARED ENTRANCE SEATING ARRANGEMENT
    • 共享入场位置安排
    • WO2015153923A1
    • 2015-10-08
    • PCT/US2015/024171
    • 2015-04-02
    • C&D ZODIAC, INC.
    • SAVIAN, Scott
    • B64D11/06
    • B64D11/0605B64D11/0015B64D11/003B64D11/0604B64D11/0606B64D11/0624B64D11/0627
    • An aircraft lounge assembly that includes an enclosure having a rear wall, first and second side walls and a forward wall that cooperate to define a seating area. The lounge assembly also includes first and second seats positioned in the seating area, and a first dividing wall positioned between the first and second seats. The first dividing wall divides the seating area into a first seat section and a second seat section. The front wall includes a shared entrance space defined therein. A first seat path is defined between the shared entrance space and the first seat section and a second seat path is defined between the shared entrance space and the second seat section.
    • 一种飞机休息室组件,其包括具有后壁,第一和第二侧壁以及配合以限定休息区的前壁的外壳。 休息室组件还包括位于休息区中的第一和第二座位以及位于第一座椅和第二座椅之间的第一分隔壁。 第一分隔壁将休息区分为第一座椅区段和第二座椅区段。 前壁包括在其中限定的共享入口空间。 第一座位路径被限定在共享入口空间和第一座椅区段之间,并且第二座位路径被限定在共享入口空间和第二座椅区段之间。
    • 18. 发明申请
    • DESIGN OPTIMIZER SYSTEM
    • 设计优化系统
    • WO2014143105A1
    • 2014-09-18
    • PCT/US2013/042895
    • 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机内部布局配置的所有可能组合的列表。 第六个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一个配置的输出,其占用最少量的座位空间,至少重量,并且包含 最大量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。
    • 20. 发明申请
    • PSU POD ASSEMBLY AND METHOD FOR USING SAME
    • PSU POD组装及其使用方法
    • WO2013123064A1
    • 2013-08-22
    • PCT/US2013/025956
    • 2013-02-13
    • C&D ZODIAC, INC.
    • SAVIAN, Scott
    • G05F1/00
    • B64D13/00B60Q3/225B60Q3/43B64D11/0015B64D11/003B64D2011/0038Y02T50/46Y10T29/49002
    • A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and. a panel positioned above and connected, to the PSU pod. The PSU pod includes at least first and second reading lights positioned, within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.
    • 被配置为定位在飞行器内部的PSU舱组件。 PSU盒组件包括PSU盒,其包括壳体,壳体包括顶部,底部以及第一,第二,第三和第四侧,其协作以限定荚内部。 位于PSU盒上方并连接到PSU盒的面板。 PSU舱包括至少第一和第二读取灯,其定位在舱内部,其被配置成将光照射在壳体下方,并且定位在壳体上或壳体中的舱灯,其配置为在壳体上方照射光。 面板包括被配置成将PSU盒组件固定到飞行器内的部件的连接器。