面向增材制造的飞机主承力结构优化设计

Optimal Design of Aircraft Main Bearing Structure for Additive Manufacturing

21世纪,我国的科学技术快速发展,在这个前提之下民用飞机交通已经大规模地投入到日常生活的使用,所以对于民用飞机的使用效率以及飞机质量等是需要工作人员大力研究的方向,特别是对于民用飞机的主承力结构以及制造材料需要利用特殊的手段来加以研究。这些方面需要从民用飞机当中结构分布的特点和结构优化等方面来分析,研究出更加科学、承力能力更加强的民用飞机主承力结构,以缩短飞机建造过程的施工周期、提高结构部件质量的措施,同时将改进后的方法做比较,更好的实现所期待的目标。

In the 21st century,the rapid development of science and technology in our country,under this premise,civil aircraft transportation has been put into daily use on a large scale,so the use efficiency and aircraft quality of civil aircraft are the directions that need to be studied by the staff.,Especially the main bearing structure and manufacturing materials of civil aircraft need to be studied by special methods.These aspects need to be analyzed from the characteristics of structural distribution and structural optimization in civil aircraft,and a more scientific and stronger main bearing structure of civil aircraft can be studied to shorten the construction period of the aircraft construction process and improve the quality of structural components.At the same time,the improved methods will be compared to achieve the desired goals better.