运载火箭非火工分离机构复用可靠性研究综述与展望

doi:10.3901/JME.260004

机械工程学报 ›› 2026, Vol. 62 ›› Issue (1): 59-78.doi: 10.3901/JME.260004

• 特邀专栏：运载火箭机构技术 • 上一篇

扫码分享

运载火箭非火工分离机构复用可靠性研究综述与展望

撒国栋^1,2,3, 王栋^1,2, 刘振宇^1,2, 孙嘉诚^1,2, 侯明杰^1,2, 李志男^1,2, 谭建荣^1,2

1. 浙江大学CAD&CG全国重点实验室杭州 310027;
2. 浙江大学机械工程学院杭州 310058;
3. 浙江大学宁波国际科创中心宁波 315100

收稿日期:2025-04-11 修回日期:2025-07-23 发布日期:2026-02-13
作者简介:撒国栋，男，1990年出生，博士，副教授，硕士研究生导师。主要研究方向为复杂装备智能设计与数字孪生。E-mail：sgd@zju.edu.cn
王栋，男，2001年出生，博士研究生。主要研究方向为复杂装备可靠性分析与优化设计、人工智能与大数据、产品数字化设计。E-mail：dongwang24@zju.edu.cn
刘振宇(通信作者)，男，1974年出生，博士，教授，博士研究生导师。主要研究方向为复杂装备智能设计、数字孪生、机器视觉。E-mail：liuzy@zju.edu.cn
孙嘉诚，男，2001年出生，博士研究生。主要研究方向为产品数字化设计。E-mail：sunjc@zju.edu.cn
侯明杰，男，1998年出生，博士研究生。主要研究方向为工程图学，智能设计。E-mail：houmj@zju.edu.cn
李志男，男，1996年出生，博士。主要研究方向为复杂产品智能设计。E-mail：zhinanlee@zju.edu.cn
谭建荣，男，1954年出生，博士，教授，博士生研究生导师，中国工程院院士，中国机械工程学会副理事长。主要研究方向为复杂装备数字化设计与制造、机械设计及理论、复杂装备健康管理等。E-mail：egi@zju.edu.cn
基金资助:
国家自然科学基金资助项目(U24B6005)。

Review and Prospect of Reuse Reliability Research on Non-pyrotechnic Separation Mechanism of Launch Vehicle

SA Guodong^1,2,3, WANG Dong^1,2, LIU Zhenyu^1,2, SUN Jiacheng^1,2, HOU Mingjie^1,2, LI Zhinan^1,2, TAN Jianrong^1,2

1. The State Key Laboratory of CAD&CG, Zhejiang University, Hangzhou 310027;
2. School of Mechanical Engineering, Zhejiang University, Hangzhou 310058;
3. Ningbo Global Innovation Center, Zhejiang University, Ningbo 315100

Received:2025-04-11 Revised:2025-07-23 Published:2026-02-13

摘要/Abstract

摘要： 在运载火箭执行任务过程中，分离机构作为关键部件，承担着有效分离火箭各级结构的任务，其可靠性直接关系到整个火箭任务的成败。近年来，随着一次性运载火箭朝向可重复使用的发展趋势，非火工分离机构因具有高可靠性和安全性等特点正得到逐步推广与应用，亟需开展复用可靠性分析以期发挥其复用性优势。详细介绍了分离机构的定义、种类与工作原理，系统性地回顾了现有机构与结构可靠性研究的方法与意义，深入探讨了现有的失效模式辨识方法与可靠性分析方法在复用型非火工分离机构上应用的不足，并展望了非火工分离机构复用可靠性研究的未来发展趋势，旨在为复用型非火工分离机构系统可靠性分析理论研究与技术创新提供参考。

关键词: 运载火箭, 复用性, 非火工分离机构, 失效模式, 可靠性

Abstract: During the mission of the launch vehicle, the separation mechanism, as a key component, is responsible for effectively detaching various stages of the rocket structure, with its reliability directly influencing the mission success rate. In recent years, as reusability has become a fundamental requirement in rocket design, non-pyrotechnic separation mechanisms have attracted increasing attention for their high reliability and safety, creating an urgent need for comprehensive reliability analysis to fully leverage their advantages in repeated applications. The definition, types, and working principles of separation mechanisms are detailed, and a systematic review of existing methods and the significance of mechanism and structural reliability research is presented. Existing failure mode identification approaches and reliability analysis methods are examined, highlighting their limitations when applied to reusable non-pyrotechnic separation mechanisms. The future development trends of reliability research on reusable non-pyrotechnic separation mechanisms are also discussed, aiming to provide a reference for theoretical research and technological innovation in the system reliability analysis of these mechanisms.

Key words: launch vehicle, reuse, non-pyrotechnic separation mechanism, failure mode, reliability

中图分类号:

撒国栋, 王栋, 刘振宇, 孙嘉诚, 侯明杰, 李志男, 谭建荣. 运载火箭非火工分离机构复用可靠性研究综述与展望[J]. 机械工程学报, 2026, 62(1): 59-78.

SA Guodong, WANG Dong, LIU Zhenyu, SUN Jiacheng, HOU Mingjie, LI Zhinan, TAN Jianrong. Review and Prospect of Reuse Reliability Research on Non-pyrotechnic Separation Mechanism of Launch Vehicle[J]. Journal of Mechanical Engineering, 2026, 62(1): 59-78.

参考文献

[1] 李东,李平岐.中国航天运输系统发展及未来趋势展[J].前瞻科技,2022,1(1):51-61.LI Dong,LI Pingqi.Development and future trend of China's space transportation system[J].Science and Technology Foresight,2022,1(1):51-61.
[2] 王国辉,张宏剑,吴会强.运载火箭非火工分离机构技术发展与展望[J].宇航学报,2023,44(3):334-347.WANG Guohui,ZHANG Hongjian,WU Huiqiang.Development and prospects of non-pyrotechnic separation mechanism technology for launch vehicles[J].Journal of Astronautics,2023,44(3):334-347.
[3] 宋征宇,黄兵,汪小卫,等.重复使用航天运载器的发展及其关键技术[J].前瞻科技,2022,1(1):62-74.SONG Zhengyu,HUANG Bing,WANG Xiaowei,et al.Development and key technologies of reusable launch vehicle[J].Science and Technology Foresight,2022,1(1):62-74.
[4] 龙乐豪,王国庆,吴胜宝,等.我国重复使用航天运输系统发展现状及展望[J].国际太空,2019(9):4-10.LONG Lehao,WANG Guoqing,WU Shengbao,et al.The development status and prospect of China's reusable space transportation system[J].Space International,2019(9):4-10.
[5] 杜涛,许晨舟,王国辉,等.人工智能气动特性预测技术在火箭子级落区控制项目的应用[J].宇航学报,2021,42(1):61-73.DU Tao,XU Chenzhou,WANG Guohui,et al.Application of artificial intelligence aerodynamic characteristic prediction technology to rocket sub-stage drop zone control project[J].Journal of Astronautics,2021,42(1):61-73.
[6] NASA-STD-7003 Pyroshock test criteria[S].NASA Technical Standard,1999.
[7] 袁晗,王小军,张宏剑,等.重复使用火箭着陆结构稳定性分析[J].力学学报,2020,52(4):1007-1023.YUAN Han,WANG Xiaojun,ZHANG Hongjian,et al.Stability analysis of reusable launch vehicle landing structure[J].Chinese Journal of Theoretical and Applied Mechanics,2020,52(4):1007-1023.
[8] 张宏剑,于兵,吴会强,等.运载火箭机构技术发展研究[J].导弹与航天运载技术(中英文),2023(6):1-9.ZHANG Hongjian,YU Bing,WU Huiqiang,et al.Launch vehicle mechanism technology development study[J].Missiles and Space Vehicles,2023(6):1-9.
[9] YUE H H,YANG Y F,LIU Y F,et al.Research progress of space non-pyrotechnic low-lock connection and separation technology (SNLT):A review[J].Chinese Journal of Aeronautics,2022,35(11):113-154.
[10] 李东,杨云飞,胡鹏祥,等.运载火箭多体动力学建模与仿真技术研究[J].宇航学报,2021,42(2):141-149.LI Dong,YANG Yunfei,HU Pengxiang,et al.Launch vehicle multi-body dynamics modeling and simulation technology research[J].Journal of Astronautics,2021,42(2):141-149.
[11] 吴瑞德,常英珂,陈小松,等.基于形状记忆合金的分离装置驱动机构研究[J].火工品,2020(5):10-13.WU Ruide,CHANG Yingke,CHEN Xiaosong,et al.Research on the driving mechanism of separation device based on shape memory alloy[J].Explosives,2020(5):10-13.
[12] 宋征宇,潘豪,王聪,等.长征运载火箭飞行控制技术的发展[J].宇航学报,2020,41(7):868-879.SONG Zhengyu,PAN Hao,WANG Cong,et al.Development of Long March launch vehicle flight control technology[J].Journal of Astronautics,2020,41(7):868-879.
[13] 袁晗,王小军,牟宇,等.火箭返回制导动力着陆段的自适应启动方法[J].宇航学报,2022,43(7):890-901.YUAN Han,WANG Xiaojun,MOU Yu,et al.Adaptive powered descent initiation of rocket return guidance[J].Journal of Astronautics,2022,43(7):890-901.
[14] 罗剑武,葛智君,陈克澎.复杂系统可靠性评估方法研究综述[J].电子产品可靠性与环境试验,2023,41(6):122-130.LUO Jianwu,GE Zhijun,CHEN Kepeng.A review of reliability assessment methods for complex systems[J].Electronic Products Reliability and Environmental Testing,2023,41(6):122-130.
[15] 何春全,严楠,叶耀坤.导弹级间火工分离装置综述[J].航天返回与遥感,2009,30(3):70-77.HE Chunquan,YAN Nan,YE Yaokun.A review of missile-level pyrotechnic separation devices[J].Aerospace Return and Remote Sensing,2009,30(3):70-77.
[16] 金旭东,葛金玉,段德高,等.导弹现代结构设计[M].北京:国防工业出版社,2007:369.JIN Xudong,GE Jinyu,DUAN Degao,et al.Modern missile structural design[M].Beijing:National Defense Industry Press,2007:369.
[17] 王凯民,温玉全.军用火工品设计技术[M].北京:国防工业出版社,2006.WANG Kaimin,WEN Yuquan.Military pyrotechnic design technology[M].Beijing:National Defense Industry Press,2006.
[18] 叶天源,王毅,汪锡发,等.水下爆炸螺栓设计探讨[J].水雷战与舰船防护,2007,15(4):11-14.YE Tianyuan,WANG Yi,WANG Xifa,et al.Discussion on underwater explosion bolt design[J].Mine Warfare and Ship Protection,2007,15(4):11-14.
[19] MOON S N.Apparatus for restraining and releasing missile using rigid sphere:U.S.Patent 6,286,409[P].2001-09-11.
[20] 高滨,李忠刚,马景.分离螺母的关键设计参数分析[J].航天返回与遥感,2001,22(2):63-65.GAO Bin,LI Zhonggang,MA Jing.Analysis of key design parameters of separation nuts[J].Aerospace Return and Remote Sensing,2001,22(2):63-65.
[21] 张营,杨树彬,王键,等.直推式低冲击分离装置的设计[J].火工品,2007(6):33-34.ZHANG Ying,YANG Shubin,WANG Jian,et al.Design of direct-push low-impact separation device[J].Explosives,2007(6):33-34.
[22] 朱维亮,张文峰.一种新型导弹级间分离机构研究[J].航天返回与遥感,2005,26(1):53-57.ZHU Weiliang,ZHANG Wenfeng.Research on a novel missile-level separation mechanism[J].Aerospace Return and Remote Sensing,2005,26(1):53-57.
[23] 徐福,吕玉连,金德兴,等.无污染炸药索分离技术[J].中国空间科学技术,1982(2):50.XU Fu,LÜ Yulian,JIN Dexing,et al.Pollution-free explosive cord separation technology[J].Chinese Journal of Space Science and Technology,1982(2):50.
[24] 奥比托科学公司.易碎连接分离系统:CN1089225[P].1994-07-13.Obito Scientific.Fragile connection separation system:CN1089225[P].1994-07-13.
[25] 张顺杰,王露斯,聂超,等.空间大载荷石蜡驱动器研制[J].北京航空航天大学学报,2017,43(5):1038-1044.ZHANG Shunjie,WANG Lusi,NIE Chao,et al.Development of paraffin drive for large space loads[J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(5):1038-1044.
[26] 赫志亮,于兵,宋保永,等.一种涡卷弹簧分离螺母装置设计及仿真分析[J].宇航总体技术,2020,4(5):65-70.HE Zhiliang,YU Bing,SONG Baoyong,et al.Design and simulation analysis of a volute spring separation nut device[J].Astronautical Systems Engineering Technology,2020,4(5):65-70.
[27] PEFFER A,DENOYER K,FOSNESS E,et al.Development and transition of low-shock spacecraft release devices[C]//2000 IEEE Aerospace Conference.Proceedings (Cat.No.00TH8484).IEEE,2000,4:277-284.
[28] 常新,张振华,杨泽涛,等.运载火箭气液连接器锁紧及解锁方案技术探讨[J].导弹与航天运载技术,2021(5):99-103.CHANG Xin,ZHANG Zhenhua,YANG Zetao,et al.Launch vehicle gas-hydraulic connector locking and unlocking scheme technology discussion[J].Missiles and Space Vehicles,2021(5):99-103.
[29] HOU Yu,ZHANG Ming,NIE Hong.Analysis of sensitive parameters affecting unlocking force of finger lock in landing gear[J].International Journal of Aerospace Engineering,2021:1-19.
[30] GALL K,LAKE M,HARVEY J,et al.Development of a shockless thermally actuated release nut using elastic memory composite material[C]//44th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.2003:1582.
[31] 范新中,肖耘.飞船整流罩纵向解锁机构设计与动力学[J].宇航学报,2004,25(5):479-483.FAN Xinzhong,XIAO Yun.Design and dynamics of the mechanical-driven lock used in the spaceship fairing[J].Journal of Astronautics,2004,25(5):479-483.
[32] EURROCKOT.Rockot user's guide[R].Bremen,Germany:EURROCKOT Launch Services GmbH,2011.
[33] 吴晗玲,胡振兴,张志峰,等.一种基于锁钩机构联动的非火工分离装置:CN201610909284.5[P].2018-11-23.WU Hanling,HU Zhenxing,ZHANG Zhifeng,et al.A non-pyrotechnic separation device based on hook-lock mechanism linkage:CN201610909284.5[P].2018-11-23.
[34] OHB.OHB Sweden and Exolaunch sign hardware agreement to deploy MATS satellite into orbit[EB/OL].(2022-11-16)[2023-02-16].https://www.spacequip.eu/2022/11/16/ohband-exolau-nch-sign-hardware-agreement-to-deploy-mats-satelliteinto-orbit/.
[35] HOLEMANS W.Lessons learned developing separation systems for small satellites[C]//20th Annual AIAA/USU Conference on Small Satellites,Logan,UT,USA.2006:1.
[36] 盖玉先,梁潇,杨帅,等.非火工包带式星箭分离技术研究进展[J].机械设计与制造,2018(1):136-139.GAI Yuxian,LIANG Xiao,YANG Shuai,et al.Research progress of non-pyrotechnic clamp-band separation technology[J].Machinery Design & Manufacture,2018(1):136-139.
[37] 郭欣,朱仕尧,刘观日,等.刚性包带式星箭连接装置解锁分离过程动力学分析[J].振动与冲击,2021,40(8):150-156.GUO Xin,ZHU Shiyao,LIU Guanri,et al.Separation dynamic analysis of a rigid-clamp-band-type satellite- rocket connection device[J].Journal of Vibration and Shock,2021,40(8):150-156.
[38] ZHAO Yong,YUE Honghao,YANG Fei,et al.A high thrust density voice coil actuator with a new structure of double magnetic circuits for CubeSat deployers[J].IEEE Transactions on Industrial Electronics,2021,69(12):13305-13315.
[39] PUIG-SUARI J,TURNER C,AHLGREN W.Development of the standard CubeSat deployer and a CubeSat class PicoSatellite[C]//2001 IEEE aerospace conference proceedings (Cat.No.01TH8542).IEEE,2001:1/347-1/353.
[40] HIHOUD M,PAGÈS A,BENOIT C,et al.BRUCE-electromagnetic actuated pin puller[C]//Proceedings of the 13th International Conference on New Actuators & 7th International Exhibition on Smart Actuators and Drive Systems.Bremen,WFB Wirtschaftsförderung Bremen GmbH,Bremen,Germany.2012:18-20.
[41] 姜晗.基于涡卷弹簧缠绕自锁性能的锁紧释放装置研制[D].哈尔滨:哈尔滨工业大学,2016.JIANG Han.Development of a locking release device based on the self-locking performance of volute coil spring winding[D].Harbin:Harbin Institute of Technology,2016.
[42] 叶耀坤,柳元青,丁锋,等.分瓣解锁机构冲击特性分析与优化[J].载人航天,2021,27(3):367-372.YE Yaokun,LIU Yuanqing,DING Feng,et al.Analysis and optimization of impact characteristics of release device with segmented nut[J].Manned Spaceflight,2021,27(3):367-372.
[43] 吴军,周国华,刘望.航天非火工压紧释放装置研究综述[J].航天器工程,2023,32(1):125-137.WU Jun,ZHOU Guohua,LIU Wang.A review of aerospace non-pyrotechnic compression release devices[J].Spacecraft Engineering,2023,32(1):125-137.
[44] CANTON-VEGA S,ESCANDE B,CRASSOUS S,et al.Lightweight,resettable separation nut:Non-explosive opening nut[C]//Proceedings of the 18th European Space Mechanisms and Tribology Symposium.Paris:European Space Agency,2019:1-2.
[45] 常新,张振华,杨泽涛,等.运载火箭气液连接器锁紧及解锁方案技术探讨[J].导弹与航天运载技术,2021(5):99-103.CHANG Xin,ZHANG Zhenhua,YANG Zetao,et al.Discussion on locking and unlocking schemes of launch vehicle gas-hydraulic connectors[J].Missiles and Space Vehicles,2021(5):99-103.
[46] 王雪峰.压电陶瓷驱动的解锁分离机构研究[J].机械设计与制造,2018(7):236-239.WANG Xuefeng.Research on unlocking separable structure based on piezoceramic[J].Machinery Design & Manufacture,2018(7):236-239.
[47] ZHANG Dou,LIU Liwu,LENG Jinsong,et al.Ultra-light release device integrated with screen-printed heaters for CubeSat's deployable solar arrays[J].Composite Structures,2020,232:111561.
[48] LUCY M,HARDY R,KIST E,et al.Report on alternative devices to pyrotechnics on spacecraft[C]//Proceedings of the 10th Annual AIAA/USU Conference on Small Satellites.Washington D.C.:AIAA,1996:5-16.
[49] 夏正文,李纯金.基于ADAMS的内曲线径向柱塞马达性能分析[J].机床与液压,2024,52(23):130-135.XIA Zhengwen,LI Chunjin.Performance analysis of internal curve radial piston motor based on ADAMS[J].Machine Tool & Hydraulics,2024,52(23):130-135.
[50] 张学聪,王伟,邢磊磊,等.一种海上液压夹紧钢桩装置油缸研究[J].机械管理开发,2025,40(1):128-130.ZHANG Xuecong,WANG Wei,XING Leilei,et al.Research on the oil cylinder of an offshore hydraulic clamping steel pile device[J].Mechanical Management Development,2025,40(1):128-130.
[51] 金栋平,丁鼎峰,伍霖,等.堆叠式卫星系统分离动力学关键技术与展望[J].航空学报,2025,46(5):316-341.JIN Dongping,DING Dingfeng,WU Lin,et al.Key technologies and prospects of separation dynamics for stacked satellite systems[J].Acta Aeronautica et Astronautica Sinica,2025,46(5):316-341.
[52] 张毅博,吴会强,张宏剑,等.太空探索技术公司运载火箭机构技术发展路线分析及启示[J].宇航学报,2025,46(3):631-640.ZHANG Yibo,WU Huiqiang,ZHANG Hongjian,et al.Analysis and implications of the technology development roadmap of SpaceX launch vehicle mechanisms[J].Journal of Astronautics,2025,46(3):631-640.
[53] SMITH S,DOWEN D,FOSNESS E,et al.Development of shape memory alloy (SMA) actuated mechanisms for spacecraft release applications[C]//13th AIAA/USU Conference on Small Satellites,1999.
[54] Thermal actuator technology[EB/OL].https://www.tot-ad.com/wp-content/uploads/2022/04/Thermal-Actuator-Technology-Whitepaper.pdf.
[55] IYER S,NARAYANAMURTHY V.A review of stage separation systems for launch vehicles[C]//Recent Advances in Applied Mechanics:Proceedings of Virtual Seminar on Applied Mechanics (VSAM 2021).Singapore:Springer Singapore,2022:161-181.
[56] Pyroshock test criteria[EB/OL].https://www.vibrationdata.com/tutorials_alt/NASA7003.pdf.
[57] YUE Honghao,YANG Yifei,LU Yifan,et al.Research progress of space non-pyrotechnic low-shock connection and separation technology (SNLT):A review[J].Chinese Journal of Aeronautics,2022,35(11):113-154.
[58] Eaton non-explosive actuators[EB/OL].https://cms.nacsemi.com/Images/FeaturedProducts/Eaton_Non-Explosive%20Actuators.pdf.
[59] DONG Wenjie,CAO Yingsai,OUYANG Linhan.Optimal test termination time in reliability growth management for systems with multiple failure modes[J].Reliability Engineering & System Safety,2025,263:111226.
[60] O'CONNOR P D T,KLEYNER A V.Practical reliability engineering[M].Hoboken:John Wiley & Sons,2025.
[61] DAS R,PRADHAN B.Bayesian reliability acceptance sampling plans under interval censoring[J].Communications in Statistics-Theory and Methods,2024,54(6):1676-1701.
[62] LIN Qingyuan,ZHAO Yong,LIU Yuming,et al.Optimization of assembly parameters for composite bolted joints aiming at time-varying bearing reliability improvement[J].Composite Structures,2025,363:119113.
[63] GRABILL N,WANG S,OLAYINKA H A,et al.AI-augmented failure modes,effects,and criticality analysis (AI-FMECA) for industrial applications[J].Reliability Engineering & System Safety,2024,250:110308.
[64] 马小兵,杨军.可靠性统计分析[M].北京:北京航空航天大学出版社,2020.MA Xiaobing,YANG Jun.Reliability statistical analysis[M].Beijing:Beihang University Press,2020.
[65] 刘品,刘岚岚.可靠性工程基础[M].3版.北京:中国计量出版社,2013.LIU Pin,LIU Lanlan.Fundamentals of reliability engineering[M].3rd ed.Beijing:China Metrology Publishing House,2013.
[66] NELSON W.Accelerated testing:Statistical models,test plans,and data analyses[M].Hoboken:Wiley- Interscience,1990.
[67] 吕震宙,宋述芳,李璐祎,等.结构/机构可靠性基础[M].西安:西北工业大学出版社,2019.LÜ Zhenzhou,SONG Shufang,LI Luyi,et al.Fundamentals of structural/mechanism reliability[M].Xi'an:Northwestern Polytechnical University Press,2019.
[68] MEEKER W Q,ESCOBAR L A.Statistical methods for reliability data[M].Hoboken:Wiley,1998.
[69] ACEVEDO C H,ZHANG Xuanyi,VALDEBENITO M A,et al.Reliability analysis combining method of moments with control variates[J].Probabilistic Engineering Mechanics,2025,81:103771.
[70] CHEN Zequan,LI Guofa,HE Jialong,et al.Adaptive structural reliability analysis method based on confidence interval squeezing[J].Reliability Engineering & System Safety,2022,225:108639.
[71] NEGREIROS A C S V de,LINS I D,MOURA M J C,et al.Reliability data analysis of systems in the wear-out phase using a (corrected) q-Exponential likelihood[J].Reliability Engineering & System Safety,2020,197:106787.
[72] FAN Jiang,XU Hongbin,MENG Q,et al.A multi-layer Kriging surrogate model for the reliability analysis of variable stator vanes in aero engines[J].The Aeronautical Journal,2025,129(1331):123-143.
[73] WANG Qiang,CHEN Jin,NI Yiqing,et al.Application of Bayesian networks in reliability assessment:A systematic literature review[J].Structures,2025,71:108098.
[74] MUKHOPADHYAY K,LIU B,BEDFORD T,et al.Remaining lifetime of degrading systems continuously monitored by degrading sensors[J].Reliability Engineering & System Safety,2023,231:109022.
[75] 白碧森.多失效模式下涡轮叶片的疲劳寿命预测与可靠性分析[D].西安:西安电子科技大学,2023.BAI Bisen.Fatigue life prediction and reliability analysis of turbine blades under multiple failure modes[D].Xi'an:Xidian University,2023.
[76] 冯蕴雯,潘维煌,刘佳奇,等.基于机器学习的飞机动力装置运行可靠性[J].航空学报,2021,42(4):394-404.FENG Yunwen,PAN Weihuang,LIU Jiaqi,et al.Aircraft powerplant operational reliability based on machine learning[J].Acta Aeronautica et Astronautica Sinica,2021,42(4):394-404.
[77] LIU Han,ZHOU Jianzhong,ZHENG Yang,et al.Fault diagnosis of rolling bearings with recurrent neural network-based autoencoders[J].ISA Transactions,2018,77:167-178.
[78] LI Mingyang,WANG Zequn.Deep learning for high-dimensional reliability analysis[J].Mechanical Systems and Signal Processing,2020,139:106399.
[79] CALANDRA R,PETERS J,RASMUSSEN C E,et al.Manifold Gaussian processes for regression[C]//2016 International Joint Conference on Neural Networks (IJCNN).IEEE,2016:3338-3345.
[80] VAPNIK V N.The nature of statistical learning theory[M].Berin:Springer,1995.
[81] BREIMAN L.Random forests[J].Machine Learning,Berin:2001,45:5-32.
[82] LI Zewen,LIU Fan,YANG Wenjie,et al.A survey of convolutional neural networks:Analysis,applications,and prospects[J].IEEE Transactions on Neural Networks and Learning Systems,2021,33(12):6999-7019.
[83] GRAVES A.Long short-term memory[J].Supervised Sequence Labelling with Recurrent Neural Networks,2012(1):37-45.
[84] LI Pengzhi,PEI Yan,LI Jianqiang.A comprehensive survey on design and application of autoencoder in deep learning[J].Applied Soft Computing,2023,138:110176.
[85] CRESWELL A,WHITE T,DUMOULIN V,et al.Generative adversarial networks:An overview[J].IEEE Signal Processing Magazine,2018,35(1):53-65.
[86] 孙宇锋,赵广燕.系统可靠性建模与仿真[M].北京:北京航空航天大学出版社,2025.SUN Yufeng,ZHAO Guangyan.System reliability modeling and simulation[M].Beijing:Beihang University Press,2025.
[87] LISNIANSKI A.Extended block diagram method for a multi-state system reliability assessment[J].Reliability Engineering & System Safety,2007,92(12):1601-1607.
[88] 李明华,刘轻骑,胡云,等.航天型号小概率事件识别与控制方法[J].质量与可靠性,2023(5):29-34.LI Minghua,LIU Qingqi,HU Yun,et al.Identification and control methods for low-probability events in aerospace models[J].Quality and Reliability,2023(5):29-34.
[89] BO Yimin,BAO Minglei,DING Yi,et al.A DNN-based reliability evaluation method for multi-state series-parallel systems considering semi-Markov process[J].Reliability Engineering & System Safety,2024,242:109604.
[90] LEE J,MITICI M.An integrated assessment of safety and efficiency of aircraft maintenance strategies using agent-based modelling and stochastic Petri nets[J].Reliability Engineering & System Safety,2020,202:107052.
[91] 李淼,王磊,熊芬芬,等.可靠性工程基础[M].北京:北京理工大学出版社,2023.LI Miao,WANG Lei,XIONG Fenfen,et al.Fundamentals of reliability engineering[M].Beijing:Beijing Institute of Technology Press,2023.
[92] FORCINA A,SILVESTRI L,DI BONA G,et al.Reliability allocation methods:A systematic literature review[J].Quality and Reliability Engineering International,2020,36(6):2085-2107.
[93] YADAV O P,ZHUANG Xing.A practical reliability allocation method considering modified criticality factors[J].Reliability Engineering & System Safety,2014,129:57-65.
[94] CRUZ J A.Applicability and limitations of reliability allocation methods[R].NASA/TM-2016-218488,2016.
[95] ZHANG Yugang,YU Tianxiang,SONG Bifeng.A reliability allocation method of mechanism considering system performance reliability[J].Quality and Reliability Engineering International,2019,35(7):2240-2260.
[96] WANG Chang'an,SHI Shengbing,WU Wei.Research on reliability test method of guided ammunition[C]//201512th IEEE International Conference on Electronic Measurement & Instruments (ICEMI).IEEE,2015:136-140.
[97] LI Ziang,FU Huimin,WU Qiong.Direct assessment method for the reliability of a seat buffer mechanism in manned spacecraft[J].Journal of Mechanical Science and Technology,2025,39:3323-3332.
[98] PRESTON P F.Confidence limits for system reliability[R].AD/A-C47533,1976.
[99] BETZ W,PAPAIOANNOU I,STRAUB D.Bayesian post-processing of Monte Carlo simulation in reliability analysis[J].Reliability Engineering & System Safety,2022,227:108731.
[100] 朱炜.航天产品可靠性评估方法[M].北京:中国宇航出版社,2022.ZHU Wei.Reliability assessment methods for aerospace products[M].Beijing:China Astronautics Publishing House,2022.

运载火箭非火工分离机构复用可靠性研究综述与展望

Review and Prospect of Reuse Reliability Research on Non-pyrotechnic Separation Mechanism of Launch Vehicle

PDF

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]	张宏剑, 石玉红, 顾春辉, 徐方舟, 乐晨, 彭波, 郭嘉. 赋能运载火箭多功能化发展的机构技术与挑战[J]. 机械工程学报, 2026, 62(1): 2-17.
[2]	田保林, 杨雪聪, 刘佳行, 闫振, 于海涛, 高海波, 邓宗全. 可重复使用运载火箭着陆支腿机构技术综述[J]. 机械工程学报, 2026, 62(1): 18-40.
[3]	林撼昕, 刘才山. 运载火箭机构动力学分析方法综述[J]. 机械工程学报, 2026, 62(1): 41-58.
[4]	廖鼎, 朱顺鹏, 牛晓鹏, 何金超, 王清远. 机械结构概率疲劳研究：现状及展望[J]. 机械工程学报, 2025, 61(8): 47-74.
[5]	邓文章, 张倩, 吴乐, 杨万然, 杨春柳. 基于ESPN的柔性制造车间多层级表征建模研究[J]. 机械工程学报, 2025, 61(8): 399-412.
[6]	雷政, 姜鹏, 姚蕊, 王勇. FAST促动器可靠性增长[J]. 机械工程学报, 2025, 61(3): 251-258.
[7]	王凯, 范小宁, 余畅, 吕召国. 基于动态Kriging模型的起重机金属结构可靠性解耦优化方法[J]. 机械工程学报, 2025, 61(2): 384-394.
[8]	陈兆玮, 王浪, 李世辉, 袁密奥, 蒲前华, 杨吉忠, 陈志辉. 极端温度荷载下齿轨铁路超大坡度桥上齿轨系统可靠性研究[J]. 机械工程学报, 2025, 61(18): 267-277.
[9]	孟德彪, 杨恒飞, 杨世源, 苏晓燕, 朱顺鹏. 自适应多保真度Kriging模型辅助的一阶可靠性分析方法[J]. 机械工程学报, 2025, 61(18): 344-365.
[10]	俞水, 吴晓, 郭鹏, 王志华. 基于首次穿越PDF自适应估计的时变可靠性分析方法[J]. 机械工程学报, 2024, 60(5): 264-275.
[11]	李莹, 张嘉方, 张钊墉, 王鑫丞, 张晋, 孔祥东. 斜盘式轴向柱塞泵柱塞颈部最小直径设计[J]. 机械工程学报, 2024, 60(4): 430-437.
[12]	白鑫, 张鹏, 张哲峰, 谢里阳. 等效疲劳寿命及其在疲劳可靠性设计中的应用[J]. 机械工程学报, 2024, 60(22): 427-436.
[13]	王嘉, 姜露露, 陶友瑞, 韩旭. 交变载荷下基于电流信号的机电系统可靠性建模与评估[J]. 机械工程学报, 2024, 60(22): 437-446.
[14]	钱萍, 刘鑫雨, 陈文华, 王哲, 郭明达. 电连接器用聚氨酯胶密封件贮存可靠性建模[J]. 机械工程学报, 2024, 60(20): 361-371.
[15]	韦新鹏, 姚中洋, 宝文礼, 张哲, 姜潮. 一种基于主动学习克里金模型的证据理论可靠性分析方法[J]. 机械工程学报, 2024, 60(2): 356-368.