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面向对象的飞机概念设计系统中的重心估算
引用本文:刘虎,卢新来,王亮,武哲. 面向对象的飞机概念设计系统中的重心估算[J]. 北京航空航天大学学报, 2004, 30(9): 905-908
作者姓名:刘虎  卢新来  王亮  武哲
作者单位:1.北京航空航天大学 航空科学与工程学院, 北京 100083
摘    要:为了在飞机概念设计阶段有效而便捷地评估方案重量和静稳定裕度等特性,研究了在一个按照面向对象方式进行数据组织的计算机辅助飞机概念设计系统中进行重心及相应重量估算的措施.着重论述了重心估算部分的面向对象结构和采用的方法,尤其是根据相关部件的设计与造型特点估算燃油及起落架重心的方法.通过在设计方案的动态调整过程中估算其重量和重心,验证了该部分的适应性和可靠性,以及设计者交互地对估算的方法和结果加以控制的灵活性. 

关 键 词:重量   计算机辅助设计   飞机设计   重心   面向对象
文章编号:1001-5965(2004)09-0905-04
收稿时间:2003-06-26
修稿时间:2003-06-26

Center of gravity estimation in an object oriented aircraft conceptual design system
Liu Hu,Lu Xinlai,Wang Liang,Wu Zhe. Center of gravity estimation in an object oriented aircraft conceptual design system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(9): 905-908
Authors:Liu Hu  Lu Xinlai  Wang Liang  Wu Zhe
Affiliation:1.School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China2. School of Computer Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:In order to evaluate such characteristics as weight and static stability of proposed concepts effectively and conveniently during aircraft conceptual design, the implementation of center of gravity and associated weight estimation in an computer aided aircraft conceptual design system, whose data organization is object oriented, was studied. The emphases were placed on the object oriented structure of center of gravity estimation and methods adopted in this part, especially the methods of estimating center of gravities of fuel and landing gear based on the design and modeling of relevant components. Through conducting weight and center of gravity estimation during the process of dynamic adjustment of concepts, the adaptability and reliability of this part, as well as the flexibility of designers’ interactive controls on estimation, were validated.
Keywords:weight  computer aided design  aircraft design  center of gravity  object oriented
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