ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Structure Design and Parameter Optimization of Lightweight Composite Canister Cover
Received date: 2012-09-12
Revised date: 2012-12-17
Online published: 2013-04-23
Supported by
Ministry Level Project
The structure of a lightweight laminated composite canister cover is designed in order to propose solutions for the problems in the composite canister covers developed at present in China. Firstly an initial design of the weak structure and principal part is proposed. The structural parameters of the cover are then optimized based on the results of transient numerical simulation for the process of gas flow impact on the cover when a missile launches. The results of numerical simulation for the process of gas flow impact on the optimized cover structure verify that the the optimized cover structure satisfies the lightweight requirement while ensuring great performance of cover separation.
QIAN Yuan , ZHOU Guangming , HE Weidong , LIU Weixian . Structure Design and Parameter Optimization of Lightweight Composite Canister Cover[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013 , 34(4) : 826 -832 . DOI: 10.7527/S1000-6893.2013.0142
[1] Copeland R L, Greene R F. Protective cover or a missile nose cone: US, 3970006, 1976.
[2] Bell R E. Missile weapon system: US, 5239909, 1992.
[3] Boeglin P H. Plate-glass fitted with an explosion-cutting device: US, 4333381, 1982.
[4] Krol U B. Frangible cover assembly for missile launchers: US, 3742814, 1971.
[5] Wu J H, Wang W T, Kam T Y. Failure analysis of a frangible laminated composite canister cover. Proceedings of the Institution of Mechanical Engineers: Part G, 1999, 213: 187-195.
[6] Doane W J. Frangible fly through diaphragm for missile launch canister: US, 4498368, 1985.
[7] Zhou G M, Yuan Z W. Study of design and experiment for integrated frangible composite diaphragm cover. Journal of Astronautics, 2007, 28(3): 707-712. (in Chinese) 周光明, 袁卓伟. 整体冲破式复合材料薄膜盖的设计与实验研究. 宇航学报, 2007, 28(3): 707-712.
[8] Fu D B, Jiang Y. Opening process of friable lid of one missile. Journal of Solid Rocket Technology, 2007, 30(4): 275-277. (in Chinese) 傅德彬, 姜毅. 某导弹易碎盖的开启过程. 固体火箭技术, 2007, 30(4): 275-277.
[9] Miao P Y, Yuan Z F. Techniques for the automatic cover opening in concentric canister launcher. Transactions of Beijing Institute of Technology, 2004, 24(4): 283-285. (in Chinese) 苗佩云, 袁曾凤. 同心发射筒燃气开盖技术. 北京理工大学学报, 2004, 24(4): 283-285.
[10] Zhou G M, Jia D C, Wang X F. Design methodology and experiment for light frangible fly through diaphragm cover. Journal of Nanjing University of Aeronautics & Astronautics, 2004, 36(6): 693-696. (in Chinese) 周光明, 贾德财, 王新峰. 轻质穿透式薄膜盖的分析、设计与实验研究. 南京航空航天大学学报, 2004, 36(6): 693-696.
[11] Yuan Z W. Design analysis and testing of missile launch canister cover. Nanjing: Nanjing University of Aeronautics and Astronautics, 2005. (in Chinese) 袁卓伟. 导弹发射箱薄膜盖设计、分析与试验. 南京: 南京航空航天大学, 2005.
[12] Zhou G M, Yuan Z W. Design, manufacture and experi-ment for new-style composite frangible fly through diaphragm cover. Journal of Astronautics, 2006, 27(2): 276-280. (in Chinese) 周光明, 袁卓伟. 新型穿透式复合材料薄膜盖的设计、制作与实验. 宇航学报, 2006, 27(2): 276-280.
[13] Qian Y, Zhou G M, Yu D J, et al. Design and analysis of the weak structure for frangible composite canister covers. Acta Aeronautica et Astronautica Sinica, 2012, 33(3): 487-492. (in Chinese) 钱元, 周光明, 于殿君, 等. 复合材料易碎盖薄弱区结构设计. 航空学报, 2012, 33(3): 487-492.
[14] Fu D B, Liu Q, Chen J W, et al. Numerical simulation on missile launching procedure. Journal of Ballistics, 2004, 16(3): 11-15. (in Chinese) 傅德彬, 刘琦, 陈建伟, 等.导弹发射过程数值模拟. 弹道学报, 2004, 16(3): 11-15.
[15] Xia Z H, Chen Y, Ellyin F. A meso/micro-mechanical model for damage progression in glass-fiber/epoxy cross-ply laminates by finite-element analysis. Composites Science and Technology, 2000, 60(8): 1171-1179.
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