Aircraft structural test load lever system design is a complicated task, parametric CAD software can easily leverage design and virtual assembly. This article describes the loading lever system parametric modeling method based on Automation Technology, developed using Visual Basic the corresponding visual modeling software. Application examples show that the software interface is friendly, easy to operate, simply enter the basic parameters of the test load point, lever arranged and data files, to complete a system of levers parametric modeling, parametric design of the loading lever system to quickly achieve Plans show.

123.vbw
MSSCCPRJ.SCC
Part1.CATPart
biaomian.txt
erji.txt
ganggan1.CATPart
part
sanji.txt
siji.txt
system.frm
system.log
system.vbp
system.vbw
txt.txt
yiji.txt
基于CATIA的飞机结构试验加载杠杆系统参数化建模方法.pdf

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