The invention belongs to the field of overall design shapes of aircrafts, and relates to a rapid design method for an airplane shape. The method comprises the following steps: creating a shape design module based on CATIA software, constructing a theoretical shape of the whole aircraft, carrying out parametric modeling on each part of the aircraft, carrying out associated design, and realizing the quick and synchronous updating capability of the shape of the whole aircraft after the shape parameters of the parts are changed. The method is simple in tool, simplified in step and convenient to operate, and improves the working efficiency of shape selection design.
本发明属于飞行器总体设计外形领域,涉及一种飞机外形快速设计方法。该方法包括:基于CATIA软件创成式外形设计模块,构建飞机全机理论外形,通过对飞机各部件进行参数化建模,并进行关联设计,实现部件外形参数更改后,全机外形快速同步更新能力。本方法工具简单,步骤简化,便于操作,提高了外形选型设计工作效率。
Rapid design method for airplane profile
一种飞机外形快速设计方法
2025-04-25
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
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