鱼雷高空投送载体结构设计特性研究

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Analysis on Structural Design Characteristics of High Altitude Delivery Carrier of Torpedo

1.
The 705 Research Institute, China Shipbuilding Industry Corporation, Xi′an 710075, China
2.
Science and Technol-ogy on Underwater Information and Control Laboratory, Xi′an 710075, China

摘要: 由于现代战争的空中化进程加剧, 制空权的争夺日趋激烈, 因此高空投送鱼雷(HADT)的出现符合现代化武器的发展趋势。分析了高空投送载体在制导滑翔炸弹(GGB)及高空反潜武器概念上的应用和研制现状, 在此基础上, 比较了HADT与GGB之间的异同点, 并从刚强度、环境适应性、导航控制、“可展开”、“可分离”等5个方面探讨了鱼雷高空投送载体的结构设计特性, 提出了相应的设计策略, 为HADT的设计研发提供思路。
- 高空投送鱼雷 /
- 投送载体 /
- 结构设计特性
Abstract: The applications of the high altitude delivery carrier to guided glide bomb(GGB) and high altitude antisub-marine weapon concept, as well as the current manufacture situation of high altitude delivery carrier, are analyzed. Subsequently, the similarities and differences between high altitude delivery of torpedo (HADT) and GGB are compared. The structural design characteristics of high altitude delivery carrier of torpedo are discussed with respect to five aspects, including rigidity and intensity, environmental suitability, navigation control, “developable”, and “detachable”, and corresponding design strategies are put forward.
- high altitude delivery of torpedo(HADT) /
- delivery carrier /
- structural design characteristics

[1]	王志杰. 研制高空反潜鱼雷的必要性及关键技术[J]. 鱼雷技术, 2009, 17(3): 1-4. Wang Zhi-jie. Necessity and Key Technologies for Deve- loping High Altitude Anti-submarine Torpedo[J]. Torpedo Technology, 2009, 17(3): 1-4.
[2]	徐德民. 鱼雷自动控制系统[M]. 西安: 西北工业大学出版社, 2001.
[3]	李莉, 任茶仙, 张铎. 折叠翼机构展开动力学仿真及优化[J]. 强度与环境, 2007, 34(1): 17-21. Li li, Ren Cha-xian, Zhang Duo. Dynamic Simulation and Optimization Design of Deployment of Folding-wing[J]. Structure & Environment Engineering, 2007, 34(1): 17-21.
[4]	张石玉, 唐金兰, 任华, 等. 燃气作动筒折叠翼展开过程分析[J]. 固体火箭技术, 2010, 33(5): 481-485. Zhang Shi-yu, Tang Jin-lan, Ren Hua, et al. Analysis of Mechanical Deployment System for Combustion-gas- ac-tuated Folded Wings[J]. Journal of Solid Rocket Tech- nology, 2010, 33(5): 481-485.