天地往返飞行器大开口舱门关键技术及其解决途径

doi:10.7527/S1000-6893.2016.0243

总体设计

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

天地往返飞行器大开口舱门关键技术及其解决途径

李保江, 邵济明, 王长焕, 黄鹏

上海宇航系统工程研究所, 上海 201108

收稿日期:2016-04-20 修回日期:2016-08-26 出版日期:2017-01-10 发布日期:2016-08-30
通讯作者: 李保江,Tel.:021-24186087,E-mail:nuaalbj@163.com E-mail:nuaalbj@163.com
作者简介:李保江,男,博士,高工。主要研究方向:航天器总体设计,航天器结构与机构。Tel:021-24186087,E-mail:nuaalbj@163.com
基金资助:
国家级项目

Key technologies and solutions for large extensible door of re-entry space vehicle

LI Baojiang, SHAO Jiming, WANG Changhuan, HUANG Peng

Shanghai Institute of Aerospace Systems Engineering, Shanghai 201108, China

Received:2016-04-20 Revised:2016-08-26 Online:2017-01-10 Published:2016-08-30
Supported by:
National Level Program

摘要/Abstract

摘要：

大开口舱门是航天飞机和X-37B等天地往返飞行器不可或缺的组成部分，跨度达到了1/3~1/2飞行器机身长度，天地往返飞行器全任务周期内的载荷条件复杂和功能要求多样决定了舱门的研制难度极大。介绍了天地往返飞行器大开口舱门技术的国外研究现状，总结了大开口舱门的共性特点；提出大开口舱门研制过程中需重点突破的总体设计技术、热防护与热密封技术、重复展收技术、重复锁紧与解锁技术等关键技术，针对各项关键技术给出了可参考的解决途径。

关键词: 天地往返飞行器, 航天飞机, 航天器, 舱门, 总体设计

Abstract:

The large extensible door is an indispensable part of the re-entry space vehicle, such as space shuttle and X-37B transportation vehicle. The length of the door can reach 1/3 to 1/2 that of the airframe. The development process of the door is very difficult due to the complex environment condition and multiplicity function requirements in the full duty cycle. The state of the art of the development of large extensible door is introduced. The common characteristics of the door are given through the analysis of the space vehicle. It is summarized that the key technologies included in the overall design, the thermal protection and heat sealing technology, the repeated deploy and close technology, the repeated lock and unlock technology, etc. The related technical solutions are also given.

Key words: re-entry space vehicle, space shuttle, spacecraft, door, overall design

中图分类号:

V423

李保江, 邵济明, 王长焕, 黄鹏. 天地往返飞行器大开口舱门关键技术及其解决途径[J]. 航空学报, 2016, 37(S1): 8-15.

LI Baojiang, SHAO Jiming, WANG Changhuan, HUANG Peng. Key technologies and solutions for large extensible door of re-entry space vehicle[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 8-15.

参考文献

[1] 王鑫, 阎杰, 于云峰. 高超声速天地往返飞行器研究[J]. 测控技术, 2006, 25(7):83-86. WANG X, YAN J, YU Y F. Research on hypersonic aerospace vehicle[J]. Measurement and Control Technology, 2006, 25(7):83-86 (in Chinese).
[2] 果琳丽, 朱永贵. 空间站天地往返运输系统初探[J]. 导弹与航天运载技术, 2000(1):7-11. GUO L L, ZHU Y G. Pilot study of the space transportation system for space station[J]. Missiles and Space Vehicles, 2000(1):7-11 (in Chinese).
[3] 彭小波. 组合循环动力技术在天地往返领域的发展与应用[J]. 导弹与航天运载技术, 2013(1):78-82. PENG X B. Development of combined cycle propulsion technology in reusable launch vehicle[J]. Missiles and Space Vehicles, 2013(1):78-82 (in Chinese).
[4] 李田囡, 王小锋, 张健全. 某无人机主起落架舱门联动机构设计[J]. 机电工程技术, 2011, 40(5):111-113. LI T N, WANG X F, ZHANG J Q. Linkage design for unmanned aerial vehicle (UAV) main landing gear door[J]. Mechanical & Electrical Engineering Technology, 2011, 40(5):111-113 (in Chinese).
[5] 张锐. 某型飞机前起落架收放机构及舱门开度分析[D]. 南京:南京航空航天大学, 2011:25-28. ZHANG R. Analysis of the retraction extend mechanism and the door open size of a type of nose landing gear[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2011:25-28 (in Chinese).
[6] 刘志全, 嵇景全. 载人航天器电动兼手动舱门的研究[J]. 中国空间科学技术, 2004(4):1-7. LIU Z Q, JI J Q. Study on an electric/manual hatch for the manned space vehicles[J]. Chinese Space Science and Technology, 2004(4):1-7 (in Chinese).
[7] 刘志全, 夏祥东, 嵇景全. 载人航天器舱门周边传动锁紧释放机构的原理与特点[J]. 载人航天, 2006(2):14-23. LIU Z Q, XIA X D, JI J Q. Principle and characteristics of manned spacecraft hatch periphery drive lock release mechanism[J]. Manned Space, 2006(2):14-23 (in Chinese).
[8] 罗克韦尔国际公司. 航天飞机运输系统[M]. 张钟林, 译. 北京:航空工业出版社, 1988:15-18. Rockwell International Co. Space shuttle transportation system[M]. ZHANG Z L, translated. Beijing:Aviation Industry Press, 1988:15-18 (in Chinese).
[9] 张鲁民. 航天飞机空气动力学分析[M]. 北京:国防工业出版社, 2009:26-31. ZHANG L M. Air dynamics analysis of space shuttle[M]. Beijing:National Defence Industry Press, 2009:26-31 (in Chinese).
[10] 沈玲玲. 空天飞行器再入过程中关键热结构的热分析[D]. 西安:西北工业大学, 2006:15-18 SHEN L L. Thermal analysis of the primary hot structure for re-entry space vehicle[D]. Xi'an:Northwestern Polytechnical University, 2006:15-18 (in Chinese).
[11] 李文武. 跨大气层飞行器总体设计及优化方法研究与实现[D]. 南京:南京航空航天大学, 2008:16-18. LI W W. Research and implementation of the overall design and optimization method of the cross atmosphere aircraft[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2008:16-18 (in Chinese).
[12] 张勇. 面向控制的高超声速飞行器一体化设计[D]. 南京:南京航空航天大学, 2011:12-15. ZHANG Y. An integrated design of hypersonic vehicle based on control[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2011:12-15 (in Chinese).
[13] 邱春图, 陈振中. 高超声速飞行器热结构设计分析技术研究[J]. 飞机设计, 2012, 32(6):6-14. QIU C T, CHEN Z Z. Study of thermal-structure design and analysis for hypersonic vehicles[J]. Aircraft Design, 2012, 32(6):6-14 (in Chinese).
[14] 郭朝邦, 牛文, 李文杰. HTV-2热防护系统及热结构技术研究进展[J]. 飞航导弹, 2012(1):92-98. GUO Z B, NIU W, LI W J. Study on HTV-2 thermal protection system and thermal structure technology[J]. Missile, 2012(1):92-98 (in Chinese).
[15] DAVID E G, RAY D, HAROLD C, et al. Materials development for hypersonic flight vehicles[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2013.
[16] DAVID A S, DANIEL B L. Lightweight TUFROC TPS for hypersonic vehicles[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2006.
[17] DEMANGE J J, DUNLAP J, STEINETZ B M. Advanced control surface seal development for future space vehicles:NASA/TM-2004-212898[R]. Washington, D.C.:NASA, 2004.
[18] PATRICK H, DUNLAP J, BRUCE M S, et al. Rudder/fin seal investigations for the X-38 re-entry vehicle:NASA/TM-2000-210338[R]. Washington, D.C.:NASA,2000.
[19] 李凡, 王树浩, 陈江涛, 等. 飞行器典型热密封结构[J]. 宇航材料工艺, 2013(1):20-25. LI F, WANG S H, CHEN J T, et al. Typical high-temperature seal structure of reusable and hypersonic vehicles[J]. Aerospace Materials and Technology, 2013(1):20-25 (in Chinese).
[20] 彭祖军. 高温动密封结构设计与分析[D]. 哈尔滨:哈尔滨工业大学, 2011:12-15 PENG Z J. Structure design and analysis of high temperature dynamic seal[D]. Harbin:Harbin Institute of Technology, 2011:12-15 (in Chinese).
[21] JEFF H, LANDON M, CHRIS L, et al. The X-38 V-201 flap actuator mechanism[C]//Proceedings of the 37th Aerospace Mechanisms Symposium. Washington, D. C.:Johnson Space Center, NASA, 2004.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

天地往返飞行器大开口舱门关键技术及其解决途径

Key technologies and solutions for large extensible door of re-entry space vehicle

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	张鸿林, 罗建军, 马卫华. 基于机器学习的航天器规避目标威胁博弈决策[J]. 航空学报, 2024, 45(8): 329136-329136.
[2]	张瑞桐, 汪雷, 刘佳佳, 朱继宏. 考虑接头参数化的空间桁架轻量化设计[J]. 航空学报, 2024, 45(5): 529715-529715.
[3]	张赛, 杨震, 杜向南, 罗亚中. 基于轨道可达域的机动航天器接近威胁规避方法[J]. 航空学报, 2024, 45(4): 328778-328778.
[4]	宁铠, 吴宝林. 基于事件驱动的航天器星下点轨迹维持控制[J]. 航空学报, 2024, 45(10): 329412-329412.
[5]	刘明, 范睿超, 邱实, 曹喜滨. 基于全驱系统理论的航天器姿轨预设性能控制[J]. 航空学报, 2024, 45(1): 628313-628313.
[6]	崔凯鑫, 段广仁. 基于干扰观测器的一类组合航天器高阶全驱抗干扰控制[J]. 航空学报, 2024, 45(1): 628892-628892.
[7]	段超, 邵小东, 胡庆雷, 吴淮宁. 基于横截函数的欠驱动航天器姿态跟踪方法[J]. 航空学报, 2024, 45(1): 628910-628910.
[8]	张大蔚, 刘国平. 时变通信约束下航天器绕飞的高阶全驱预测控制方法[J]. 航空学报, 2024, 45(1): 628633-628633.
[9]	方乐言, 蒙晗, 侯明哲. 带有参数精确估计的迭代学习滑模控制及应用[J]. 航空学报, 2024, 45(1): 628889-628889.
[10]	段广全, 刘国平. 基于全驱系统方法的组合航天器位姿自适应预设性能控制[J]. 航空学报, 2024, 45(1): 628837-628837.
[11]	肖冰, 张海朝. 航天器姿态稳定强化学习鲁棒最优控制方法[J]. 航空学报, 2024, 45(1): 628890-628890.
[12]	屠园园, 王大轶, 张香燕, 李嘉兴, 黄晓峰. 航天器的可重构性与自主重构方法[J]. 航空学报, 2023, 44(23): 628855-628855.
[13]	丁玉临, 韩忠华, 乔建领, 聂晗, 宋文萍, 宋笔锋. 超声速民机总体气动布局设计关键技术研究进展[J]. 航空学报, 2023, 44(2): 626310-626310.
[14]	许闯, 吴宝林. 输入饱和下多航天器分布式固定时间输出反馈姿态协同控制[J]. 航空学报, 2023, 44(10): 327465-327465.
[15]	刘培栋, 焦博涵, 党朝辉. 面向空间引力波探测的多边形编队设计方法[J]. 航空学报, 2022, 43(S1): 726907-726907.