Structural Design and Experiment Analysis of a Morphing Wing Structure

Song Zhendong; Li Gang; Guo Bing

doi:10.16578/j.issn.1004.2539.2020.03.024

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Structural Design and Experiment Analysis of a Morphing Wing Structure

Test·Analysis | 更新时间：2022-10-20

- Structural Design and Experiment Analysis of a Morphing Wing Structure
- Journal of Mechanical Transmission Vol. 44, Issue 3, Pages: 148-154(2020)
- 作者机构：
  
  1.深圳职业技术学院机电工程学院，广东深圳 518055
  2.沈阳新松机器人自动化股份有限公司，辽宁沈阳 110168
- 作者简介：
- 基金信息：
- DOI：10.16578/j.issn.1004.2539.2020.03.024
  CLC：
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宋振东,李刚,郭冰.可变形机翼结构设计与实验分析[J].机械传动,2020,44(03):148-154.

Song Zhendong,Li Gang,Guo Bing.Structural Design and Experiment Analysis of a Morphing Wing Structure[J].Journal of Mechanical Transmission,2020,44(03):148-154.
宋振东,李刚,郭冰.可变形机翼结构设计与实验分析[J].机械传动,2020,44(03):148-154. DOI： 10.16578/j.issn.1004.2539.2020.03.024.

Song Zhendong,Li Gang,Guo Bing.Structural Design and Experiment Analysis of a Morphing Wing Structure[J].Journal of Mechanical Transmission,2020,44(03):148-154. DOI： 10.16578/j.issn.1004.2539.2020.03.024.

摘要

利用平面多闭环连杆机构，提出一种可变形机翼结构，并对该结构进行数学建模，利用结构数学模型，在Matlab中进行了机构的运动轨迹仿真分析。为了验证机构曲率调节能力及气动特性，建立了机构的三维模型，进行了运动学仿真及空气动力学仿真分析。为了获得更好的气动特性，基于传统人工鱼群优化算法，提出一种改进的人工鱼群优化算法，利用经典优化算法测试函数测试了该算法的性能。采用该优化算法对可变形机翼进行结构优化。在理论研究的基础上，加工了实验样机，并进行了相关实验测试。

Abstract

A morphing wing structure is proposed by using planar multi-closed loop linkage. The mathematical model of the structure is established. The mechanism trajectory is simulated and analyzed in Matlab by using the structural mathematical model. In order to verify the curvature adjustment ability and aerodynamic characteristics of the mechanism， a three-dimensional model of the mechanism is established， and the kinematics simulation and aerodynamics simulation analysis are carried out. In order to obtain better aerodynamic characteristics， an improved artificial fish swarm optimization algorithm is proposed based on the traditional artificial fish swarm optimization algorithm. The performance of the algorithm is tested by the classical optimization algorithm test functions. The optimization algorithm is used to optimize the morphing wing structure. On the basis of theoretical research， the experimental prototype is processed and the related experimental tests are carried out.

关键词

可变形机翼结构设计仿真分析优化算法样机实验

Keywords

Morphing wingStructure designSimulation analysisOptimization algorithmPrototypeExperiment

references

WILLIAM WG.Mission adaptive wing system for tactical aircraft［J］.Journal of Aircraft，1981，18（7）：597-602.

KUDVA N J，APPA K，JARDINE P A，et al.Overview of recent progress on the DARPA/USAF wright laboratory smart materials and structures development-smart wing program［C］.Proceedings of the Smart Structures and Materials 1997：Industrial and Commercial Applications of Smart Structures Technologies.Bellingham：SPIE，International Society for Optics and Photonics，1997，3044：24-33.

MOORED K W，BART-SMITH H.The analysis of tensegrity structures for the design of a morphing wing［J］.Journal of Applied Mechanics，2007，74（4）：668-676.

MONNER HP，SACHAU D，BREITBACH E.Design aspects of the elastic trailing edge for an adaptive wing［R］.［S.l.］：German Aerospace Center Braunschweig （Germany）Institute of Structural Mechanics，2000：1-8.

MONNER H P.Realization of an optimized wing camber by using formvariable flap structures［J］.Aerospace Science and Technology，2001，5（7）：445-455.

REED JR J L，HEMMELGARN C D，PELLEY B M，et al.Adaptive wing structures［C］.Proceedings of the Smart Structures and Materials 2005：Industrial and Commercial Applications of Smart Structures Technologies.Bellingham：SPIE，International Society for Optics and Photonics，2005，5762：132-142.

KORATKAR N A，CHOPRA I.Wind tunnel testing of a mach-scaled rotor model with trailing-edge flaps［J］.Journal of the American Helicopter Society，2001，10（1）：1-14.

SOFLA A Y N，ELZEY D M，WADLEY H N G.Two-way antagonistic shape actuation based on the one-way shape memory effect［J］.Journal of Intelligent Material Systems & Structures，2008，19（9）：1017-1027.

DANA M E，ARASH Y N，WADLEY H N G.A bio-inspired high-authority actuator for shape morphing structures［C］.Proceedings of the Smart Structures and Materials 2003：Active Matericals：Behaviorand Mechanics.Bellingham：SPIE，2003，5053：92-100.

SOFLA A Y N，MEGUID S A，TAN K T，et al.Shape morphing of aircraft wing：status and challenges［J］.Materials & Design，2010，31（3）：1284-1292.

SOFLA A Y N，ELZEY D M，WADLEY H N G.Shape morphing hinged truss structures［J］.Smart Materials & Structures，2009，18（65012）：22-39.

顾娜.基于步进电机的自适应机翼驱动系统设计［D］.南京：南京航空航天大学，2009：5-16.

GU Na.A design of a driven system for an adaptive wing based on stepping motor［D］.Nanjing：Nanjing University of Aeronautics and Astronautics，2009：5-16.

李飞.飞机自适应机翼的驱动机构研究［D］.南京：南京航空航天大学，2009：12-17.

LI Fei.Research on adaptive wing structures based on niti SMA actuator［D］.Nanjing：Nanjing University of Aeronautics and Astronautics，2009：12-17.

YIN W，FU T，LIU J，et al.Structural shape sensing for variable camber wing using FBG sensors［C］.Proceedings of the Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring 2009：Sensors and Smart Structures Technologies for Civil，Mechanical，and Aerospace Systems.Bellingham：SPIE，2009，7292：1-10.

YIN W，LIU L，CHEN Y，et al.Variable camber wing based on pneumatic artificial muscles［C］.Proceedings of the Second International Conference on Smart Materials and Nano Technology in Engineering 2009.Bellingham：SPIE，International Society for Optics and Photonics，2009，7368：1-9.

李刚，戈占堃，边弘晔.可变形机翼机构设计及分析［J］.中国新技术新产品，2018（3）：5-6.

LI Gang，GE Zhankun，BIAN Hongye.Design and analysis of morphing wing mechanism［J］.New Technology & New Products of China，2018（3）：5-6.

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