公开(公告)号：US20140278270A1

公开(公告)日：2014-09-18

申请号：US13841840

申请日：2013-03-15

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Sandesh Shetty ,  Adam Sbeglia

IPC: G06F17/50

CPC classification number: G06F17/5095 ,  B64D11/00 ,  B64D11/06 ,  G06F2217/02 ,  G06F2217/46

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20160180017A1

公开(公告)日：2016-06-23

申请号：US15059162

申请日：2016-03-02

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Sandesh Shetty ,  Roy Benjamin Sandberg

IPC: G06F17/50

CPC classification number: G06F17/5095 ,  B64D11/00 ,  B64D11/06 ,  B64F5/00 ,  G06F2217/02

Abstract: 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.

Abstract translation: 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;被配置为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。