Abstract:The thin-walledlenticular CFRP (Carbon Fiber Reinforced Plastic)space as cantilever. The two symmetry axils of cross section are taken as neutral axils respectively.Modal Testing is performed in order to obtain the natural frequency of the boom, which plays an important role in dynamic analysis. FEM model of the CFRP boom is built by ADINA, and the conditions without air and with air surrounded around are taken into consideration respectively. Thenumerical simulation results, compared with the Modal Testing results, indicate that it is necessary to concern the influence of air when the test object is a thin-walledlenticular CFRP boom which has a length of 10 meters. Parametric analysis is done to evaluate the deviation of the natural frequency under the condition of air surrounded and no-air surrounded, such as the length of the boom.The presented work is valuable to the optimization design of thin-walled lenticular CFRP boom.
康雄建1,陈务军1,邱振宇1,余征跃2,谢超3,曹争利3. 空间薄壁CFRP豆荚杆模态试验及分析[J]. 振动与冲击, 2017, 36(15): 215-221.
KANG Xiong-jian1, CHEN Wu-jun1, QIU Zhen-yu1, YU Zheng-yue2, XIE Chao3, CAO Zheng-li3. Modal Experiment and Analysis of the Thin-walled Lenticular CFRP Space Boom. JOURNAL OF VIBRATION AND SHOCK, 2017, 36(15): 215-221.
[1] 陈务军.空间可展结构体系与分析导论[M].北京:中国宇航出版社,2006:1-50.
[2] 白江波,熊峻江,高军鹏,等.可折叠复合材料豆荚杆的制备与验证[J].航空学报,2011,32(7):1217-1223.
BAI Jiang-bo, XIONG Jun-jiang, GAO Jun-peng etc. Fabrication and validation of collapsible composite lenticular tubes [J].ActaAeronauticaetAstronauticaSinica, 2011,32(7):1217-1223.
[3] 房光强,彭福军.航天器可展开支撑杆的研制及其收拢展开特性研究[J].材料工程,2009,s2:157-160.
FANG Guang-qiang,PENG Fu-jun. Fabrication and retraction/deployment testingof space deployable booms[J]. Journal of Material Engineering, 2009,s2: 157-160.
[4] 董志强,段宝岩.星载天线缠绕肋条的力学特性研究[J].西安电子科技大学学报,2001,28(6):755-758.
DONG Zhi-qiang, DUAN Bao-yan. Study of the behavior mechanics of the extendible satellite antenna with the type of twinning ribs [J]. Journal of Xidian University, 2001, 28(6): 755-758.
[5] 李瑞雄,陈务军,付功义,等.透镜式缠绕肋压扁缠绕过程数值模拟分析[J].宇航学报,2011,32(1): 224-231.
LI Rui-xiong, CHEN Wu-jun. Numerical simulation of flattening and wrapping process of lenticular wrapped-rib [J].Journal of Astronautics, 2011, 32(1): 224-231.
[6] 邹涛,陈务军,彭福军等.透镜式缠绕肋收展过程数值模拟分析[J].哈尔滨工程大学学报,2013,34(2):151-156.
ZOU Tao, CHEN Wu-jun, PENG Fu-jun etc.Numerical simulation of stowing and deployingprocess of lenticular wrapped-rib [J].Journal of Harbin Engineering University, 2013,34(2):151-156.
[7] 李瑞雄,陈务军,付功义.透镜式薄壁CFRP 管空间伸展臂轴压屈曲分析及试验[J].宇航学报,2012,33(8): 1164-1170.
LI Rui-xiong, CHEN Wu-jun, FU Gong-yi.Buckling Analysis and Experiment of Lenticular CFRP Thin-WalledTube Space Boom under Axial Compression[J].Journal of Astronautics, 2012,33(8):1164-1170.
[8] 李瑞雄,陈务军,付功义等.透镜式缠绕肋压扁缠绕过程数值模拟及参数研究[J].工程力学,2011,28(11):244-250.
LI Rui-xiong, CHEN Wu-jun. Numerical simulation and parametric study on flattening and wrapping process of lenticular wrapped-rib[J], Engineering of Mechanics,2011,28(11):244-250.
[9] 刘锦贤. 空间可展天线支撑结构热-结构分析[D].上海:上海交通大学,2013.
LIU Jing-xian. Thermal-structure Analysis for Support Structure of Deployable Space Antenna[D]. Shanghai: Shanghai Jiaotong University, 2013.
[10] Herbeck L, Leipold M, Sickinger C, et al. Development and test of deployable ultra-lightweightCFRP-boomsfor a solar sail[C]//Spacecraft Structures, Materials and Mechanical Testing. 2001, 468: 107.
[11] Sickinger C, Herbeck L, Breitbach E. Structural engineering on deployable CFRP booms for a solar propelled sailcraft[J]. ActaAstronautica, 2006, 58(4): 185-196.
[12] Irwin R J, Veen J A V, Buchner-Santos E, et al. Low-Mass Deployable Spacecraft Booms[J]. AIAA Paper, 2010, 8926: 2010.
[13] Chu Z Y, Lei Y A. Design theory and dynamic analysis of a deployable boom[J]. Mechanism and Machine Theory, 2014, 71: 126-141.
[14] Straubel M, Block J, Sinapius M, et al. Deployable composite booms for various gossamer space structures[C]//52ndAIAA/asme/asce/ahs/asc Structures, Structural Dynamics, and Materials Conference. 2011.
[15] 李华峰. 空间结构数值风洞模拟与流固耦合风致响应[D].上海交通大学,2008.
LI Hua-feng. Numerical wind tunnel simulation and fluid-structure interaction analysis for space structure. [D]. Shanghai Jiao Tong University,2008.