基于非等距偏置的纤维铺放路径规划算法

doi:10.7527/S1000-6893.2014.0337

Abstract

Abstract:

Due to their high strength-to-weight and stiffness-to-weight ratios, ablative resistance and corrosion resistance, composite materials are widely used in aeronautics, astronautics and automation industries. Fiber placement is a key method for fabricating composite structures, which is also the fastest growing and most efficient composite manufacturing technique. To manufacture composites, especially complex structures, the materials must be placed on the mold precisely. To address this problem, a path planning algorithm for complex surface is proposed using the differential geometry. With the determined roller location and orientation, the initial path is constructed on the basis of surface-plane intersection strategy. Then, the roller paths, covering the whole mold, are formulated by offsetting surface curves non-equidistantly. The generated paths have a good performance in that not only are the tows placed on the mold completely, but also the tow-number information is included. Namely, the precise modeling of composite part is achieved in theory. By conducting path simulations in MATLAB, the validity of the path planning algorithm is verified.

Key words: composites, fiber placement, differential geometry, path planning algorithm, number of tows

CLC Number:

V261
TP391

YAN Long, WANG Fazhan, SHI Yaoyao. Path planning algorithm for fiber placement based on non-equidistant offsets[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(11): 3715-3723.

References

[1] Wu L Y. Current status of advanced aerospace composites[C]//Proceedings of the 13th National Conference on Epoxy Resins Application. Tianjin:China Epoxy Resins Applied Technology Institute, 2009:117-132(in Chinese).吴良义.航空航天先进复合材料现状[C]//第十三次全国环氧树脂应用技术学术交流会论文集.天津:中国环氧树脂应用技术学会, 2009:117-132.
[2] Helth J. Inside manufacturing:Automated tape-laying excels for F-22's wing skin panels[J]. High Perform Composites, 1999, 7(5):27-30.
[3] Shao Z X. Research on key technology of fiber placement machine[D]. Harbin:Harbin Institute of Technology, 2010(in Chinese).邵忠喜.纤维铺放装置及其铺放关键技术研究[D].哈尔滨:哈尔滨工业大学, 2010.
[4] Huan D J. Fundamental research on CAD/CAM technology of composite material automated placement[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2010(in Chinese).还大军.复合材料自动铺放CAD/CAM关键技术研究[D].南京:南京航空航天大学, 2010.
[5] Olsen H, Craig J. Automated composite tape-lay-up using robotic devices[C]//Proceedings of the IEEE International Conference on Robotics and Automation. Piscataway, NJ:IEEE Press, 1993:291-297.
[6] Shirinzadeh B, Foong C, Tan B. Robotic fiber placement process planning and control[J]. Assembly Automation, 2000, 20(4):313-320.
[7] Shirinzadeh B, Alici G, Foong C, et al. Fabrication process of open surfaces by robotic fiber placement[J]. Robotics and Computer-Integrated Manufacturing, 2004, 20(1):17-28.
[8] Shirinzadeh B, Cassidy G, Oetomo D, et al. Trajectory generation for open-contoured structures in robotic fiber placement[J]. Robotics and Computer-Integrated Manufacturing, 2007, 23(4):380-394.
[9] Lin F J. Trajectory planning of automatic fiber placement of composite material parts with free profile[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2005(in Chinese).林福建.自由型面复合材料零件铺丝束成型轨迹规划[D].南京:南京航空航天大学, 2005.
[10] Shao G J. Research on integrated CAD/CAE/CAM system for automated tow placement[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2006(in Chinese).邵冠军.自动铺丝束CAD/CAE/CAM技术研究[D].南京:南京航空航天大学, 2006.
[11] Xiong W L, Xiao J, Wang X F, et al. Algorithm of adaptive path planning for automated placement on meshed surface[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2):434-441(in Chinese).熊文磊,肖军,王显峰,等.基于网格化曲面的自适应自动铺放轨迹算法[J].航空学报, 2013, 34(2):434-441.
[12] An L L, Zhou Y, Zhou L S. Composite fiber placement path planning and fiber number determination[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(3):745-750(in Chinese).安鲁陵,周燚,周来水.复合材料纤维铺放路径规划与丝数求解[J].航空学报, 2007, 28(3):745-750.
[13] Duan Y G, Yan X F, Li C, et al. Effect of material and shape of compaction roller on the voids and compaction uniformity in fiber placement process[J]. Acta Aeronauticaet Astronautica Sinica, 2014, 35(4):1173-1180(in Chinese).段玉岗,闫晓丰,李超,等.压辊材料及形状对纤维铺放压紧效果的影响[J].航空学报, 2014, 35(4):1173-1180.
[14] Krishnan S, Manocha D. An efficient surface intersection algorithm based on lower-dimensional formulation[J]. ACM Transactions on Graphics, 1997, 16(1):74-106.
[15] Cassidy G. Robotic fiber placement:Trajectory generation for open contoured structures[D]. Melbourne:Monash University, 2003.
[16] Limaiem A, Tronchu F. Geometric algorithms for the intersection of curves and surfaces[J]. Computers & Graphics, 1995, 19(3):391-403.
[17] Zhu X X. Modeling technology of free-form curve and surface[M]. Beijing:Science Press, 2000:332-334(in Chinese).朱心雄.自由曲线曲面造型技术[M].北京:科学出版社, 2000:332-334.
[18] Mei X M. Differential geometry[M]. Beijing:Higher Education Press, 2010:87-91(in Chinese).梅向明.微分几何[M].北京:高等教育出版社, 2010:87-91.
[19] Patrikalakis N. Surface-to-surface intersections[J]. Computer Graphics & Applications 1993, 13(1):89-95.
[20] Li Q Y, Wang N C, Yi D Y. Numerical analysis[M]. Wuhan:Huazhong University of Science and Technology Press, 2006:79-86(in Chinese).李庆扬,王能超,易大义.数值分析[M].武汉:华中科技大学出版社, 2006:79-86.
[21] Schueler K, Miller J, Hale R. Approximate geometric methods in application to the modeling of fiber placed composite structures[J]. Journal of Computing and Information Science in Engineering, 2004, 4(3):251-256.

Path planning algorithm for fiber placement based on non-equidistant offsets

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Wenbin JIA, Lei FANG, Gen ZHANG, Jian SHI, Zekan HE, Haijun XUAN. Optimal design of fracture toughness for CNT⁃epoxy composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 428971-428971.
[2]	Hongyu YIN, Yu WU, Tianjiao LIANG. Cooperative path planning for patrol coverage of fixed wing UAV [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 328944-328944.
[3]	Chunyun ZHANG, Xiongbin CHEN, Jian LIU, Miao CUI. Prediction of thermo⁃physical properties of inorganic⁃organic hybrid phenolic aerogel composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 428848-428848.
[4]	Lingcai HUANG. Review of nondestructive testing methods for fiber⁃reinforced polymer composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529697-529697.
[5]	Qian YANG, Yanzhe WANG, Di YANG, Zezhong LI, Weiwei QU. Prediction and planning of automatic laying speed for fiber reinforced composite materials based on data⁃driven model [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 429313-429313.
[6]	Jiqiang GAN, Xiaoping WANG. Surface defect detection of fiber placement based on virtual sample generation [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 428624-428624.
[7]	Hongyue WANG, Bing WANG, Guodong FANG, Songhe MENG. Digital element modelling and analysis of 2.5D woven shallow cross bending composites [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 227478-227478.
[8]	Yang SUN, Jian HUANG, Chenchen HAN, Zhenqiang ZHAO, Haili ZHOU, Fangfang SUN, Chao LI, Chao ZHANG, Liquan ZHANG. Comparison of in-plane mechanical properties of 2D and 3D woven composites [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 428267-428267.
[9]	Chao TANG, Wenjun XIE, Peiyu YUAN, Zonghong XIE. Development and verification of a conformal electrothermal deicing functional structure for leading edge of airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 427872-427872.
[10]	Zhiwen LI, Changchun CAI, Huan YU, Zhifeng XU, Zhenjun WANG, Rongxing LI. Bending properties of composite braided structure T⁃shaped parts of C_f/Al composite material [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(10): 427510-427510.
[11]	KANG Shuo, KE Zhenzheng, WANG Xuan, ZHU Weidong. Detection method of defects in automatic fiber placement based on fusion of infrared and visible images [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 425187-425187.
[12]	ZOU Qi, YE Yiyun, JIAO Junke, WU Zhisheng, XU Zifa, ZHANG Wenwu. Performance analysis of carbon fiber reinforced thermalsetting composite-titanium alloy laser joint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 625037-625037.
[13]	YANG Zhangang, SUI Zheng, ZHANG Qihao, LIU Jianying. Voltage drop in composite aircraft grounding and current return network [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 324859-324859.
[14]	ZHAO Chenwei, MAO Junkui, TU Zecan, QIU Penglin. Thermal analysis methods for high-temperature ceramic matrix composite components: Review and prospect [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 24126-024126.
[15]	WEN Liwei, YU Kun, HUAN Huasong. Finite element numerical simulation of stitched composite T-joint under tensile load [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224231-224231.