双壳体混合驱动水下滑翔机结构原理及水动力性能研究

刘健; 周广礼; 彭嘉澍; 朱猛; 李国庆; 余祖耀

doi:10.11993/j.issn.2096-3920.2023-0150

双壳体混合驱动水下滑翔机结构原理及水动力性能研究

doi: 10.11993/j.issn.2096-3920.2023-0150

刘健^1,,
周广礼^2,,
彭嘉澍^1,,
朱猛^1,,
李国庆^1,,
余祖耀^1, ,

1.
华中科技大学船舶与海洋工程学院, 湖北武汉, 430074
2.
海军研究院, 北京, 100161

详细信息

作者简介:
刘健：刘　健(1996-), 男, 在读硕士, 主要研究方向为仿真计算、结构分析等

通讯作者:
余祖耀(1972-), 男, 副教授, 博士, 主要研究方向为液压控制及结构分析

中图分类号: TJ630; U674.941
计量
- 文章访问数: 763
- HTML全文浏览量: 21
- PDF下载量: 40
- 被引次数: 0
出版历程
- 收稿日期: 2023-11-28
- 修回日期: 2024-01-04
- 录用日期: 2024-01-10
- 网络出版日期: 2024-01-18

Research on Structural Principle and Hydrodynamic Performance of Double-Hull Hybrid Powered Underwater Glider

LIU Jian^1
,,
ZHOU Guangli^2
,,
PENG Jiashu^1
,,
ZHU Meng^1
,,
LI Guoqing^1
,,
YU Zuyao^{1
, ,}

1.
School of Naval Architecture & Ocean Engineering, Huazhong University of Science and Technology, Wuhan 430074, China
2.
Naval Research Academy, Beijing 100161, China

摘要

摘要: 混合驱动水下滑翔机虽兼具典型水下滑翔机及传统航行器的优点, 但存在能耗高、不利回收等缺点, 且在快速推进模式下, 滑翔翼的存在不仅会增加航行阻力, 降低航行稳定性, 也不利于滑翔机回收布放。针对此, 提出一种双壳体混合驱动水下滑翔机, 其滑翔翼与传统固定水平翼不同之处在于滑翔机可根据实际需求进行收放, 以实现对能源的合理分配, 从而提高水下滑翔机的综合航行性能。此外, 详细介绍了该滑翔机的工作模式、系统组成以及滑翔翼收放原理, 并设计了一种蜗轮蜗杆滑翔翼收放装置, 建立相应的收放机构技术方案, 在此基础上通过数值仿真方法进行了滑翔翼水动力性能分析, 得到了合理的机载配置方案。
- 水下滑翔机 /
- 双壳体 /
- 混合驱动 /
- 滑翔装置 /
- 水动力性能
Abstract: Although the hybrid powered underwater glider has the advantages of both typical underwater gliders and traditional vehicles, it also has disadvantages such as high energy consumption and inconvenient recovery. In the rapid propulsion mode, the existence of wings not only increases navigation resistance and reduces navigation stability but also is not conducive to the recovery and deployment of gliders. In view of this, a dual-hull hybrid powered underwater glider was proposed. The wings of the glider can be retracted according to the actual needs, which is different from the traditional fixed horizontal wing, so as to realize the reasonable distribution of energy and improve the comprehensive navigation performance of underwater gliders. In addition, the working mode, system composition, and wing retracting principle of the glider were introduced in detail, and a worm gear and worm glide wings retracting device was designed. The corresponding retracting mechanism was established. On this basis, the hydrodynamic performance of the wings was analyzed by numerical simulation method, and a reasonable shipborne configuration scheme was obtained.
- underwater glider /
- double-hull /
- hybrid powered /
- gliding wing /
- hydrodynamic performance

HTML全文

图 1 双壳体混合驱动水下滑翔机滑翔翼工作示意图

Figure 1. Working state of the double-hull hybrid powered underwater glider wings

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图 2 双壳体混合驱动水下滑翔机工作流程示意图

Figure 2. Work flow of the double-hull hybrid powered underwater glider

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图 3 双壳体混合驱动水下滑翔机内外壳体连接示意图

Figure 3. The connection between the inner and outer shells of the double-hull hybrid powered glider

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图 4 双壳体混合驱动水下滑翔机内部模块结构图

Figure 4. Internal module structure of the double-hull hybrid powered underwater glider

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图 5 滑翔翼驱动系统机构运动简图

Figure 5. Motion of glider wings drive system mechanism

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图 6 滑翔翼驱动系统控制框图

Figure 6. Block diagram of glider wings drive system control

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图 7 计算域边界尺寸设置

Figure 7. Settings of calculate domain boundary size

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图 8 双壳体混合驱动水下滑翔机网格划分

Figure 8. Meshing of double-hull hybrid powered underwater glider

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图 9 网格无关性验证

Figure 9. Grid independence verification

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图 10 收放翼轴向布置相对位置示意图

Figure 10. Relative position of the axial arrangement of the retracting wings

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图 11 升阻比随轴向距离变化曲线

Figure 11. Lift-drag ratio varies with axial distance

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图 12 收放翼垂向布置相对位置示意图

Figure 12. Relative position of vertical arrangement of retracting wings

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图 13 升阻比和俯仰力矩随垂向距离变化曲线

Figure 13. Lift-drag ratio and pitching moment varies with vertical distance

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图 14 后掠角定义示意图

Figure 14. Definition of the sweep angle

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图 15 升阻比和俯仰力矩随后掠角变化曲线

Figure 15. Lift-drag ratio and pitching moment varies with sweep angle

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