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
    • 135. 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。
    • 137. 发明申请
    • FASTENER SYSTEM
    • 紧固系统
    • WO2015148690A1
    • 2015-10-01
    • PCT/US2015/022522
    • 2015-03-25
    • C&D ZODIAC, INC.
    • MCCLURE, Richard
    • B64C1/00
    • F16B2/12B64C1/066B64C1/403B64D11/02F16B2/10F16B2/185F16B5/0607F16B5/0621F16B21/065F16B21/09Y10T24/45707
    • A fastener system that includes a female fastener assembly with a housing having a channel defined therein and a switch member movable within the channel between removing and fastening positions. The switch member includes a receiver portion having a post opening defined therein and a switch portion. The housing includes a lower opening. The post opening includes a removing portion that is aligned with the lower opening when the switch member is in the removing position and a fastening portion that is aligned with the post opening when the switch member is in the fastening position. The system also includes a male fastener assembly having a post with a slot therein. The post is received through the lower opening in the housing and the post opening so that the slot is aligned with the channel. The slot receives a portion of the receiver portion when the switch member is in the fastening position.
    • 一种紧固件系统,其包括具有限定在其中的通道的壳体的阴紧固件组件和在移除和紧固位置之间的通道内可移动的开关构件。 开关构件包括具有限定在其中的柱形开口的接收器部分和开关部分。 壳体包括下开口。 后开口包括当开关构件处于移除位置时与下开口对准的移除部分和当开关构件处于紧固位置时与柱塞开口对准的紧固部分。 该系统还包括具有其中具有狭槽的柱的阳紧固件组件。 柱通过壳体中的下开口和柱开口接收,使得槽与通道对准。 当开关构件处于紧固位置时,狭槽接收接收器部分的一部分。
    • 139. 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。
    • 140. 发明申请
    • READING LIGHT
    • 阅读灯
    • WO2014110286A1
    • 2014-07-17
    • PCT/US2014/010919
    • 2014-01-09
    • C&D ZODIAC, INC.
    • ORSON, Benjamin, RichardJIN, ZhaoMECKE, Christian
    • B60Q3/02
    • F21V15/012B64D11/00B64D47/02B64D2011/0053
    • A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions.
    • 一种照明组件,其包括限定外部壳体轴线的外部壳体,限定内部壳体轴线的内部壳体和定位在所述内部壳体中的轻型构件。 外壳包括具有前开口的前表面和限定具有截头球形的调节空腔的内表面。 内壳体具有截头球形并且至少部分地容纳在调节空腔内。 内壳体在其中限定一个光凹槽,并且包括其中限定有孔的前盖。 前盖至少部分地限定光凹部。 光构件限定光轴。 光轴和内壳体轴线不是同轴的并且不平行并且在它们之间形成一个角度。 内壳体在原位置和多个调节位置之间是可调节的。