固体力学与飞行器总体设计

基于三维参数化模型构建的飞机重量重心快速估算方法

  • 罗明强 ,
  • 魏城龙 ,
  • 刘虎 ,
  • 武哲
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  • 北京航空航天大学 航空科学与工程学院, 北京 100191
罗明强 男, 博士, 讲师。主要研究方向: 飞机总体设计技术及相关领域。 Tel: 010-82329491-308 E-mail: lmq19810222@163.com;魏城龙 男, 硕士研究生。主要研究方向: 飞机设计。 Tel: 010-82339801 E-mail: bataxi@163.com;刘虎 男, 博士, 副教授。主要研究方向: 飞机总体设计, 虚拟仿真技术等。 Tel: 010-82339801 E-mail: liuhu@buaa.edu.cn;武哲 男, 博士, 教授, 国家突出贡献专家。主要研究方向: 飞机总体设计, 隐身技术等。 Tel: 010-82317557 E-mail: wuzhe@beihangonline.com

收稿日期: 2012-08-27

  修回日期: 2012-10-18

  网络出版日期: 2013-03-29

基金资助

部级项目

Rapid Estimation Method for Aircraft Weight and Center of Gravity Based on 3-D Parametric Modeling

  • LUO Mingqiang ,
  • WEI Chenglong ,
  • LIU Hu ,
  • WU Zhe
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  • School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received date: 2012-08-27

  Revised date: 2012-10-18

  Online published: 2013-03-29

Supported by

Ministry Level Project

摘要

针对飞机总体设计阶段重量重心(c.g.)估算的专业要求、设计方案反复调整的特点,提出了基于三维参数化建模的重量重心快速估算方法,从而实现后续的快速参数化调整。基于该方法的分析流程,通过分析飞机外形建模和结构、系统重量建模的工作对象和专业逻辑,对各个重量组成及其建模过程进行了参数化描述和流程定义,用于指导完成整个设计分析系统的开发实现。最后,通过算例演示了基于三维参数化建模进行重量重心快速估算的步骤。

本文引用格式

罗明强 , 魏城龙 , 刘虎 , 武哲 . 基于三维参数化模型构建的飞机重量重心快速估算方法[J]. 航空学报, 2013 , 34(3) : 566 -573 . DOI: 10.7527/S1000-6893.2013.0093

Abstract

According to the requirements of frequent estimation and adjustment of weight and center of gravity (c.g.) during aircraft conceptual design, a method based on 3-D parametric modeling is proposed to realize rapid weight and c.g. estimation and adjustment by editing relevant parameters. Based on the method, the parameters used to describe the model and the process of modeling are determined by analyzing the object and logic of aircraft modeling, so that the system used for model design and weight analysis can be developed. Finally, a case study is presented to show the procedure of weight and c.g. estimation using the method proposed by this paper.

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