基于APDL语言的机翼结构优化设计与分析  

Wing Structure Optimization Design and Analysis Based on APDL Language

作　　者：谢帅[1] 李飞[1] 吴波[1] 

机构地区：[1]中国飞行试验研究院,陕西西安710089

出　　处：《航空科学技术》2017年第8期16-20,共5页Aeronautical Science & Technology

摘　　要：机翼结构设计是飞机结构设计的重要环节之一,通常在气动外形确定之后进行。根据机翼气动外形,首先对元件进行二维布局设计,确定机翼结构形式及梁、肋、缘条、油箱等的位置,初步给出各构件尺寸大小,然后在ANSYS中应用APDL语言,建立合理的有限元模型,进行静力学计算分析,进一步使用子问题逼近算法对机翼结构进行强度和变形约束下的结构优化,得到重量最轻的结构设计。结果表明,使用APDL这种参数化的建模语言进行机翼结构优化是可行的,能有效提高结构优化和设计阶段的工作效率。Wing structure design is an important part of aircraft design, which usually starts after aerodynamic configuration is confirmed. This paper made 2D configuration design of parts according to aerodynamic configuration firstly, confirmed wing structure type and the location of beam, rib, flange, oil box, etc, defined the size of parts preliminary, built reasonable finite element model using APDL in ANSYS, made statics computation and analysis, made wing structure optimization by sub-problem approximation method under constraints of stiffness and strength, got the most lightest structure weight finally. The results show that it is feasible to make wing structure optimization using APDL language, it also can increase structure efficiency and design efficiency.

关 键 词：APDL语言 ANSY3 优化设计 有限元 机翼结构 

分 类 号：V224[航空宇航科学与技术—飞行器设计]