首页> 外国专利> MATHEMATICA CODE GENERATING DEVICE FOR GENERALIZED ONE-DIMENSIONAL COMPRESSIBLE FLOW AND CONTROLLING METHOD FOR THE SAME

MATHEMATICA CODE GENERATING DEVICE FOR GENERALIZED ONE-DIMENSIONAL COMPRESSIBLE FLOW AND CONTROLLING METHOD FOR THE SAME

机译:广义一维可压缩流的数学代码生成装置及其控制方法

摘要

The present invention provides an one dimensional compressive flow analysis code generating device using Mathematica and a control method thereof including a second process in which a code writing module writes about basic components of a fuel system designed by a designing module with an one dimensional compressive flow analysis code by using a Mathematica method after a first process; a third process in which an analyzing module predicting and outputting a change according to a flight state and a correlation between a pipe and each component installed in the basic components of the fuel system by analyzing the one dimensional compressive flow analysis code written by the code writing module after the second process; and a fourth process in which a design modifying module modifies and simulates the basic components of the fuel system by using prediction change values in the basic components analyzed by the analyzing module, then compares and analyzes the result, and re-modifies the basic components according to the fuel system according to the comparison and analysis result in order to complete the final design for the basic components of the system. According to the present invention, as a code analyzing an one dimensional compressive flow with the Mathematica providing various functions is generated for the modification and development of basic components of a flight, the basic components of the flight are designed by verifying the accuracy of simulation by integrating the basic components so that a cost for malfunction detection can be reduced besides reducing a costly mass Rig test.
机译:本发明提供了一种使用Mathematica的一维压缩流分析代码生成装置及其控制方法,该方法包括第二过程,其中代码编写模块编写由具有一维压缩流分析的设计模块设计的燃料系统的基本组件。在第一个过程之后通过使用Mathematica方法进行编码;第三过程,其中分析模块通过分析由代码编写器编写的一维压缩流分析代码,根据飞行状态以及管道与燃料系统基本组件中安装的每个组件之间的相关性预测并输出变化。第二步后的模块;第四过程,设计修改模块利用分析模块所分析的基本部件中的预测变化值对燃料系统的基本部件进行修改和模拟,然后对结果进行比较和分析,并根据需要对基本部件进行重新修改。根据比较和分析结果向燃料系统中添加燃料,以完成系统基本组件的最终设计。根据本发明,当生成具有Mathematica提供各种功能的一维压缩流的代码以修改和开发飞行基本成分时,通过验证模拟的准确性来设计飞行基本成分。集成了基本组件,因此除了减少昂贵的大规模装备测试之外,还可以降低故障检测的成本。

著录项

  • 公开/公告号KR101409362B1

    专利类型

  • 公开/公告日2014-06-20

    原文格式PDF

  • 申请/专利权人 KOREA AEROSPACE INDUSTRIES LTD.;

    申请/专利号KR20130040333

  • 发明设计人 LEE CHANG SOO;

    申请日2013-04-12

  • 分类号G06F17;G06F17/10;

  • 国家 KR

  • 入库时间 2022-08-21 15:40:40

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