• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2017, Vol. 53 ›› Issue (13): 125-135.doi: 10.3901/JME.2017.13.125

• 数字化设计与制造 • 上一篇    下一篇

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仿生轻质结构在飞机大开口区的应用及其优化设计

郭策1, 陆振玉2, 吴元琦1   

  1. 1. 南京航空航天大学航天学院 南京 210016
    2. 中国科学院长春光学精密机械与物理研究所 长春 130033
  • 出版日期:2017-07-05 发布日期:2017-07-05
  • 作者简介:

    郭策(通信作者),女,1971年出生,教授,博士研究生导师。主要研究方向为仿生多功能结构设计、结构拓扑优化。

    E-mail:guozc@nuaa.edu.cn

  • 基金资助:
    * 国家重点基础研究发展计划(973计划,2011CB302106)、国家自然科学基金(51175249,51105201,51475230)、航空基金(2013ZF52072)和教育部博士点基金(20123218110010)资助项目; 20160616收到初稿,20161229收到修改稿;

The Application of Biomimetic Lightweight Sandwich Panel to the Aircraft Structure with Large Cutout and Its Optimum Design

GUO Ce1, LU Zhengyu2, WU Yuanqi1   

  1. 1. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 2100162. Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033
  • Online:2017-07-05 Published:2017-07-05

摘要:

将一种新型的仿甲虫鞘翅轻质结构应用于飞机大开口区的筋板结构设计,根据飞机大开口区对结构静/动态性能和散热性能的要求,分别构造目标函数,并采用拉丁超立方试验设计方法确定样本点数,建立有限元参数化模型进行仿真计算,利用响应面法得到各目标函数的响应面拟合函数,之后设定结构的多功能协同优化目标,并通过线性搜索法进行协同优化设计,优化后计算得到仿生轻质结构的散热性能、抗压刚度分别是优化前的14.3倍和2.1倍,动态性能指标得到明显改善,在相同载荷条件下结构减重11%;进一步以飞机大开口区加筋结构的一阶屈曲因子和最大位移作为优化约束条件,并以结构总质量最小为优化目标,构造各自响应面拟合函数,基于遗传算法优化筋板结构整体布局。优化后开口区加筋结构总质量减少15%,屈曲因子为1.02,较优化前提高21%,结构最大位移为12.1 mm,较优化前减少20%,优化效果显著。

关键词: 布局优化, 大开口区, 多功能协同优化, 响应面法, 仿生轻质结构

Abstract:

A novel beetle’s elytra-inspired lightweight structure is used as the stiffeners of the skin-stiffened structure with large cutout in the aircraft. According to the requirements on the mechanical and thermal properties of such stiffeners, the objective functions are built respectively, which all are nonlinear, so the response surface method is chosen to obtain the approximation models of the three objective functions and the sample points are determined by Latin hypercube sampling experimental design method, whose properties are figured out through building FEM parameterized model and numerical simulation. Based on the approximation models, the multi-function cooperative optimization design is performed and linear search method is used to obtain the optimized properties of the inspired structure, whose heat dissipation and compressive resistance ability are 14.3 and 2.1 times respectively as the non-optimized ones, also its dynamic property is improved dramatically, and its weight is lighten by 11% with same load bearing. Furthermore, taking the first-order buckling factor and the maximum displacement of this skin-stiffened structure with large cutout as two constrain conditions, and total structure weight as objective function, the response surface method is applied again to obtain the approximation models, and the genetic algorithm is used to work out the optimized layout of stiffeners. According to optimization results, the total structure weight is lessened by 15%, at the same time, the first-order buckling factor is 1.02, increased by 21%, and the maximum displacement is 12.1 mm, decreased by 20%, demonstrating the optimization design is very effectively.

Key words: large opening area, layout optimization, multi-functional optimization, response surface method, bio-inspired structure