飞机机身气动载荷自动分载研究  

Research on automatic distribution of aircraft fuselage aerodynamic load

作　　者：李文博 张浩成 马靖楠 LI Wenbo;ZHANG Haocheng;MA Jingnan(Chengdu Aircraft Industrial(Group)Co.,Ltd.,Chengdu 610091,China)

机构地区：[1]航空工业成都飞机工业(集团)有限责任公司,成都610091

出　　处：《成都航空职业技术学院学报》2023年第4期44-46,共3页Journal of Chengdu Aeronautic Polytechnic

摘　　要：为实现飞机机身气动载荷的自动分载,采用VB进行软件开发,输入为气动专业提供的机身总载和机身气动载荷分布形态参数,输出为静强度专业加载所用的机身各个框站位所分的集中载荷。软件操作方便,有效提升了机身气动载荷分载的效率和质量。To realize the automatic distribution of aerodynamic load on aircraft fuselage,the software is developed by VB.The input is the total load and the distribution parameters of the fuselage aerodynamic load provided by the pneumatic specialty,and the output is the concentrated load on each frame station of the fuselage used for loading by the static strength specialty.This software is easy to operate,which effectively improves the efficiency and quality of the aerodynamic distribution of the fuselage.

关 键 词：飞机机身 气动载荷 自动分载 

分 类 号：V215.1[航空宇航科学与技术—航空宇航推进理论与工程]