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空天防御  2023, Vol. 6 Issue (2): 28-34    
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  先进结构设计与制造技术 本期目录 | 过刊浏览 | 高级检索 |
面向增材制造的导弹结构优化设计综述
柯林达1,2, 张小龙1, 崔哲1,2, 顾铭峰1,2, 赖彩芳1, 刘勇1
1. 上海航天精密机械研究所,上海 201600; 2.上海金属材料近净成形工程技术研究中心,上海 201600
Review of Missile Structural Optimization Design for Additive Manufacturing
KE Linda1,2, ZHANG Xiaolong1, CUI Zhe1,2, GU Mingfeng1,2, LAI Caifang1, LIU Yong1
1. Shanghai Spaceflight Precision Machinery Institute, Shanghai 201600, China;2. Shanghai Engineering Technology Research Center of Near-Net-Shape Forming for Metallic Materials, Shanghai 201600, China
全文: PDF(1107 KB)  
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摘要 随着增材制造技术的发展和应用不断深入,创新导弹结构设计与增材制造技术的协同融合,必定是导弹研发领域发展突破的重要方向。从静力学设计、动态结构设计、耦合动力学3个方面,探讨了先进增材制造技术在导弹结构优化设计中的应用。导弹结构优化涉及动态特性、气动弹性、力热耦合等多个方面,增材制造凭借其独特优势,突破了传统的设计模式和加工瓶颈,进一步实现了航天武器装备结构的轻量化、体积小型化、功能集成化。
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关键词 导弹结构设计增材制造激光选区熔化    
Abstract:With the development of AM (additive manufacturing) technology, the integration of innovative structure design and AM technology must be the critical direction of breakthrough development in missile development and structural design. This paper discussed the application of advanced additive manufacturing technology in missile structure optimization in three parts: the static design, the dynamic structure design and the coupling dynamics. Since the optimization of missile structure involves dynamic characteristics, aeroelasticity, mechanical-thermal coupling etc., relying on its unique advantages, AM technology can break through the traditional design mode and the processing bottleneck, and can further realize the lightweight, small size and functional integration of space weapon equipment.
Key wordsmissile structure design    additive manufacturing    selective laser melting
收稿日期: 2022-12-30      出版日期: 2023-07-06
ZTFLH:  TJ 760.3  
作者简介: 柯林达(1986—),男,博士,高级工程师,主要研究方向为基于增材制造的航天器结构优化设计与制造。
引用本文:   
柯林达, 张小龙, 崔哲, 顾铭峰, 赖彩芳, 刘勇. 面向增材制造的导弹结构优化设计综述[J]. 空天防御, 2023, 6(2): 28-34.
KE Linda, ZHANG Xiaolong, CUI Zhe, GU Mingfeng, LAI Caifang, LIU Yong. Review of Missile Structural Optimization Design for Additive Manufacturing. Air & Space Defense, 2023, 6(2): 28-34.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2023/V6/I2/28

参考文献
[1] 丁晓红, 张横, 沈洪. 高速飞行器结构优化及增材制造研究进展[J]. 空天防御, 2023, 6(2): 1-11.
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