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
    • 2. 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。
    • 3. 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。
    • 4. 发明申请
    • DESIGN OPTIMIZER SYSTEM AND METHODS
    • 设计优化系统和方法
    • WO2016141101A1
    • 2016-09-09
    • PCT/US2016/020511
    • 2016-03-02
    • C & D ZODIAC, INC.
    • SAVIAN, ScottSHETTY, SandeshSANDBERG, Roy, Benjamin
    • B60N2/00B64D11/06G06F17/50
    • G06F17/50B64D11/06
    • A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.
    • 一种用于确定飞机设计布局的计算机化系统。 该系统包括:输入模块,被配置为接收指示第一参数的第一值的第一输入数据;包括多个特征设置的第一特征数据库;配置成搜索第一特征数据库并选择特征设置的特征搜索模块 基于所述第一参数的第一值,包括控制机身的设计布局的多个规则的中央数据库,以及与所述中央数据库通信并被配置为基于所选择的特征生成最佳设计布局的优化模块 设置。