一种联翼式平流层飞艇的总体设计

doi:10.3969/j.issn.1009-086x.2020.01.001

现代防御技术 ›› 2020, Vol. 48 ›› Issue (1): 1-10.DOI: 10.3969/j.issn.1009-086x.2020.01.001

• 专栏 • 下一篇

一种联翼式平流层飞艇的总体设计

韩庆, 乔梁, 秦琪

西北工业大学航空学院,陕西西安 710072

收稿日期:2019-10-14 修回日期:2019-11-14 出版日期:2020-02-20 发布日期:2021-01-20
作者简介:韩庆(1969-),男,山东高青人。副教授,博士,主要从事飞行器总体综合设计以及飞机生存力研究。通信地址:710072 陕西省西安市友谊西路127号 E-mail:hanq925@nwpu.edu.cn

Overall Design of a Joint Wing Stratospheric Airship

HAN Qing, QIAO Liang, QIN Qi

Northwestern Polytechnical University,School of Aeronautics,Shaanxi Xi′an 710072,China

Received:2019-10-14 Revised:2019-11-14 Online:2020-02-20 Published:2021-01-20

摘要/Abstract

摘要： 对比分析现有平流层飞艇,提出了一种常规流线型升力艇加中间机翼设计的联翼式平流层飞艇,对其进行了总体设计、关键部件设计和数字化建模,经过气动可行性分析以及参数敏感性分析,对方案进行了初步验证,验证结果显示该设计具有可行性。该飞艇可在临近空间范围内长时间续航,为远程侦察、情报探测、国土勘测、灾情获取、通信等提供搭载平台,对未来临近空间飞艇设计具有参考价值。

关键词: 平流层飞艇, 联翼, 临近空间, 气动分析, 参数敏感性分析

Abstract: Comparing and analyzing the existing stratospheric airships, a joint-type stratospheric airship with a conventional streamlined lift boat and intermediate wing is proposed. The concept, key components and digital model are designed. Through aerodynamic feasibility and parameter sensitivity analyzing, the feasibility of the preliminary scheme is proposed. The airship can maintain long-term life in the vicinity of the space, enabling remote reconnaissance, intelligence detection, land survey, disaster acquisition, and communication. The low cost and other advantages have reference value for future spacecraft design.

Key words: stratospheric airship, joint wing, near space, aerodynamic analysis, parameter sensitivity analysis

中图分类号:

V274

韩庆, 乔梁, 秦琪. 一种联翼式平流层飞艇的总体设计[J]. 现代防御技术, 2020, 48(1): 1-10.

HAN Qing, QIAO Liang, QIN Qi. Overall Design of a Joint Wing Stratospheric Airship[J]. Modern Defense Technology, 2020, 48(1): 1-10.

参考文献

[1] 祝明,陈天,梁浩全,等.临近空间浮空器研究现状与发展展望[J].国际航空,2016(1):22-25.
ZHU Ming,CHEN Tian,LIANG Hao-quan,et al.Research Status and Development Prospects of Adjacent Space Aerostats[J].International Aviation,2016(1):22-25.
[2] 王彦广,李伟志,黄灿林,等.平流层飞行器技术的最新发展[J].航天返回与遥感,2019,40(2):2-3.
WANG Yan-guang,LI Wei-zhi,HUANG Can-lin,et al.The Latest Development of Stratospheric Aircraft Technology[J].Space Return and Remote Sensing,2019,40 (2):2-3.
[3] 黄宛宁,栗颖思,周书宇,等.现代浮空器军事应用[J].科技导报,2017,35(15):20-27.
HUANG Wan-ning,LI Ying-si,ZHOU Shu-yu,et al.Military Application of Modern Aerostats[J].Science and Technology Review,2017,35 (15):20-27.
[4] 徐文.平流层飞艇蒙皮材料力学性能研究[D].上海:上海交通大学,2017.
XU Wen.Study on Mechanical Properties of Stratosphe-ric Airship Skin Material [D].Shanghai:Shanghai Jiaotong University,2017.
[5] 赵新路.平流层飞艇总体设计优化方法研究[D].长沙:国防科学技术大学,2016.
ZHAO Xin-lu.Research on the Overall Design Optimization Method of Stratospheric Airship[D].Changsha:National University of Defense Technology,2016
[6] 王飞,王伟志.半硬式与软式平流层飞艇结构静力性能比较[J].航天返回与遥感,2017,38(5):18-28.
WANG Fei,WANG Wei-zhi.Comparison of Static Performance of Semi-Rigid and Soft Stratospheric Airships[J].Aerospace Return & Remote Sensing,2017,38(5):18-28.
[7] 孟军辉,张艳博,吕明云.平流层飞艇蒙皮材料织物纤维拔出过程分析[J].北京航空航天大学学报,2014,40(8):1149-1153.
MENG Jun-hui,ZHANG Yan-bo,LÜ Ming-yun.Analysis of Fabric Fiber Extraction Process of Stratospheric Airship Skin Material[J].Journal of Beijing University of Aeronautics & Astronautics,2014,40(8):1149-1153.
[8] 刘军虎,刘振辉,纪雪梅,等.平流层飞艇蒙皮材料的研究现状[J].信息记录材料,2016,17(2):1-5.
LIU Jun-hu,LIU Zhen-hui,JI Xue-mei,et al.Research Status of Stratospheric Airship Skin Materials[J].Information Recording Materials,2016,17(2):1-5.
[9] 宋笔锋,王海峰,杨旭东,平流层飞艇推进系统研究进展与挑战[C]∥第三届高分辨率对地观测学术年会,北京,2014:343-352.
SONG Bi-feng,WANG Hai-feng,YANG Xu-dong.Research Progress and Challenges of Stratospheric Airship Propulsion System[C]∥The 3rd High Resolution Earth Observation Academic Conference,Beijing,2014:343-352.
[10] 金龙,刘沛清,胡天翔.平流层飞艇推进系统研究进展与挑战[C]∥2019年全国工业流体力学会议,北京,2019:166-175.
JIN Long,LIU Pei-qing,HU Tian-xiang.Research Progress and Challenges of Stratospheric Airship Propulsion System[C]∥National Industrial Fluid Mechanics Conference,Beijing,2019:166-175.
[11] 刘新强,贺卫亮.平流层飞艇动力推进系统的分析与设计[J].航空动力学报,2015,30(6):1407-1412. LIU Xin-qiang,HE Wei-liang.Analysis and Design of the Stratospheric Airship Power Propulsion System[J].Journal of Aerospace Power,2015,30(6):1407-1412.
[12] 武伟,倪勇.平流层飞艇太阳能电池研究现状[J].中国高新区,2018(12):14-16.
WU Wei,NI Yong.Research Status of Stratospheric Airship Solar Cells[J].China High-Tech Zone,2018(12):14-16.
[13] 李天娥,孙晓颖,武岳,等.平流层飞艇气动阻力的参数分析[J].工程力学,2019,36(1):248-256.
LI Tian-wei,SUN Xiao-ying,WU Yue,et al.Parameter Analysis of Aerodynamic Drag of Stratospheric Airships[J].Engineering Mechanics,2019,36(1):248-256.
[14] 赵达,刘东旭.平流层飞艇研制现状、技术难点及发展趋势[J].航空学报,2016,37(1):45-56.
ZHAO Da,LIU Dong-xu.Development Status,Technical Difficulties and Development Trend of Stratospheric Airships[J].Journal of Aeronautics,2016,37(1):45-56.
[15] 南海阳,韩晓明,刘洪引,等.国外临近空间飞行器发展现状及趋势[J].飞航导弹,2014(10):3-8.
NAN Hai-yang,HAN Xiao-ming,LIU Hong-yin,et al.Development Status and Trend of Foreign Space Vehicles[J].Flying Missile,2014(10):3-8.

一种联翼式平流层飞艇的总体设计

Overall Design of a Joint Wing Stratospheric Airship

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 11

编辑推荐

Metrics

本文评价

[1]	李宏宇, 尹童, 敦晓彪. 临近空间高超声速武器发展概况与防御体系研究[J]. 现代防御技术, 2022, 50(6): 1-10.
[2]	张清南, 李昂, 陈晓岚, 范伯钧, 李佳欣. 两种充气碟形囊体结构力学性能比较研究[J]. 现代防御技术, 2021, 49(6): 29-35.
[3]	王鹏飞, 罗畅, 白炎. 临近空间高超声速飞行器进展及防御策略分析[J]. 现代防御技术, 2021, 49(6): 16-21.
[4]	薄钧天, 王国宏, 于洪波, 张敬艳. 大时空差条件下高超声速目标检测关联算法[J]. 现代防御技术, 2021, 49(5): 56-64.
[5]	李君龙, 周荻, 王冠, 陈晓波, 秦雷. 临近空间目标跟踪与预报技术研究[J]. 现代防御技术, 2021, 49(3): 1-12.
[6]	刘尊洋, 陈天宇. 临近空间高超声速飞行器预警探测系统探索[J]. 现代防御技术, 2020, 48(6): 89-95.
[7]	叶泽浩, 毕红葵, 段敏, 李凡, 朱源才. 控制律预测的再入滑翔飞行器轨迹预测算法[J]. 现代防御技术, 2018, 46(6): 7-14.
[8]	赵凯丽, 高火涛, 曹婷. 临近空间高超声速目标跟踪IMMCPF算法[J]. 现代防御技术, 2018, 46(5): 94-101.
[9]	喻晨龙, 谭贤四, 王红, 曲智国, 谢非. 临近空间高超声速滑翔弹跟踪模型[J]. 现代防御技术, 2018, 46(4): 99-106.
[10]	钟玲玲. 临近空间低动态涡扇动力飞行器应用发展研究[J]. 现代防御技术, 2018, 46(4): 8-13.
[11]	韩春耀, 熊家军, 张凯. 无动力滑翔高超声速飞行器轨迹预测方法[J]. 现代防御技术, 2018, 46(3): 146-151.