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基于结构设计的自调节铺放轨迹规划算法
引用本文:文立伟,李俊斐,王显峰,肖军.基于结构设计的自调节铺放轨迹规划算法[J].航空学报,2013,34(7):1731-1739.
作者姓名:文立伟  李俊斐  王显峰  肖军
作者单位:南京航空航天大学材料科学与技术学院,江苏南京,210016
基金项目:民机预研专项;国家自然科学基金(50905088);国家科技重大专项(2010ZX04016-013);中央高校基本科研业务费专项资金(NS2012112);国家商用飞机制造工程技术研究中心创新基金(SAMC11-JS-07-222)
摘    要:通过分析预浸带/纱在曲面上的铺放工艺性,提出以轨迹测地曲率作为铺放工艺性测度,构建一种基于结构设计的自调节轨迹规划算法,兼顾自动铺放中的铺放工艺性和结构设计要求.该算法是在满足结构设计的前提下,将预浸带/纱轨迹从结构设计所确定的方向按特定方式向测地线方向偏转,从而减小预浸带/纱的变形.本文以固定角度法作为结构设计准则、以最大容许偏转角法定义修正函数,以此为例阐述具体算法及实施过程.基于Visual C++平台,进行C++和SQL混合编程,以某型进气道为模型进行了算法仿真,并进行了进气道和锥壳的铺放试验.结果表明:容许偏转角的增大有助于缓解预浸带/纱的变形.

关 键 词:复合材料  自动铺放  轨迹规划  结构设计  铺放工艺性  自调节算法

Adjustment Algorithm Based on Structural Design for Automated Tape Laying and Automated Fiber Placement
WEN Liwei , LI Junfei , WANG Xianfeng , XIAO Jun.Adjustment Algorithm Based on Structural Design for Automated Tape Laying and Automated Fiber Placement[J].Acta Aeronautica et Astronautica Sinica,2013,34(7):1731-1739.
Authors:WEN Liwei  LI Junfei  WANG Xianfeng  XIAO Jun
Institution:College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:By analyzing the placeable characteristic of prepreg tapes/tows on curved surfaces, the geodesic curvature of the trajectory is taken as the evaluation parameter of the processing characteristic of prepreg tapes/tows. An adjustment algorithm is proposed based on structural design for Automated Tape Laying (ATL) and Automated Fiber Placement (AFP), in order to strike a balance between the requirements of the placing process and structural design. On the premise of meeting the structural design demand, the novel algorithm diverts the placement direction from the original one (which is generated according to structural design) to the adjusted one (which is closer to the geodesic direction) in a specific way, aiming at releasing the strains in prepreg tapes/tows. In this paper, the algorithm is described in detail for the case when the structure is designed in the fixed fiber orientation method and the diversion follows the rule of maximum deflection angle. In addition, the algorithm is programmed in Visual C++ and SQL language by C++. Through the verification on an aeroplane inlet model and the experiments on the inlet and the cone structure, it is demonstrated that increasing the deflection angle can relieve the deformation of the prepereg tapes/tows.
Keywords:composite materials  automated tape laying &  automated fiber placement  trajectory planning  structural design  placeable characteristic  adjustment algorithm
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