PDF下载 分享
[1]杜大华,穆朋刚,田川,等.液体火箭发动机管路断裂失效分析及动力优化[J].火箭推进,2018,44(03):16-22.
 DU Dahua,MU Penggang,et al.Failure analysis and dynamics optimization of pipeline for liquid rocket engine[J].Journal of Rocket Propulsion,2018,44(03):16-22.
点击复制

液体火箭发动机管路断裂失效分析及动力优化

参考文献/References:

[1] BACHSCHMID N, PENNACCHI P, VANIA A, et al. Case studies of fault identification in power plant large rotating machinery [C]// 6th IFToMM-Conference on Rotor Dynamics, Austrilia:Sydney, 2002:191-200.
[2] 权凌霄, 孔祥东. 液压管路流固耦合振动机理及控制研究现状与发展[J]. 机械工程学报, 2015, 51(18):175-183.
[3] 张立翔, 黄文虎. 输流管道流固耦合振动研究进展[J]. 水动力学研究与进展, 2000, 15(3):366-379.
[4] 徐云飞, 李锋. 液体火箭发动机充液导管流固耦合动力学特性[J]. 航空动力学报, 2017, 32(6):1523-1529.
[5] 陈香林, 周文禄. 压力管道流固耦合振动特性分析[J]. 火箭推进, 2007, 33(5):27-31.
CHEN Xianglin, ZHOU Wenlu. Vibration characteristic analysis of pressure pipes with fluid-structure interaction [J]. Journal of rocket propulsion, 2007, 33(5): 27-31.
[6] 尹志勇, 钟荣. 管路系统振动噪声控制技术研究现状与展望[J]. 舰船科学技术, 2006, 28(2):23-29.
[7] 梁向东. 船舶管路中高频振动成因分析及控制策略研究[J]. 噪声与振动控制, 2009(3):101-103.
[8] 卢金丽, 黄超广. 飞机液压燃油管路系统振动故障模式、机理及排除方法[J]. 振动工程学报, 2008, 21(S):78-82.
[9] 李会娜, 高庆. 发动机长悬壁管路动力学特性优化及试验验证[J]. 航天器环境工程, 2015, 32(4):400-403.
[10] LI Z J, LIAO H T, COIT D W. A two-stage approach for multi-objective decision making with application to system reliability optimization [J]. Reliability engineering and system safety, 2009, 94:1585-1592.
[11] EAMON C, RAIS-ROHANI M. Integrated reliability and sizing optimization of a large composite structure [J]. Marine structure, 2009, 22: 315-334.
[12] VALDEBENITO M A, SCHUELLER G I. Reliability-based optimization considering design variables of discrete size. Engineering Structure, 2010, 32: 2919-2930.
[13] 李士杰. 1Cr18Ni9Ti钢的低周疲劳特性研究[J]. 核动力工程, 1991, 12(2):34-37.
[14] CALVI A, AGLIET G, ALBUS J, et al. ECSS-E-HB-32-26A space engineering spacecraft mechanical loads analysis handbook [M]. [S.l.]: ECSS Secretariat ESA-ESTEC, 2013.

相似文献/References:

[1]陈 佳,顾铖璋,林仁邦,等.主结构与贮箱共承力航天器推进平台设计[J].火箭推进,2020,46(04):67.
 CHEN Jia,GU Chengzhang,LIN Renbang,et al.Design of spacecraft propulsion platform with main structure and tank bearing together[J].Journal of Rocket Propulsion,2020,46(03):67.
[2]毛 凯,李昌奂,张 聃,等.高压液氧涡轮泵孔型/蜂窝阻尼密封的设计[J].火箭推进,2021,47(02):47.
 MAO Kai,LI Changhuan,ZHANG Dan,et al.Design of the hole-pattern/honeycomb seals in the high-pressure liquid oxygen turbopump[J].Journal of Rocket Propulsion,2021,47(03):47.
[3]梁文栋,许健,刘博,等.球型调节阀液动力矩特性仿真及优化设计[J].火箭推进,2024,50(03):53.[doi:10.3969/j.issn.1672-9374.2024.03.006]
 LIANG Wendong,XU Jian,LIU Bo,et al.Simulation and optimization design of hydrodynamic torque characteristics of ball-type regulating valves[J].Journal of Rocket Propulsion,2024,50(03):53.[doi:10.3969/j.issn.1672-9374.2024.03.006]

备注/Memo

收稿日期:2017-09-27
基金项目:国家自然科学基金青年基金(11702204); 装备预研共用技术和应用基础(2017ZZB·YY4001Da)
作者简介:杜大华(1977—),男,高级工程师,博士,研究领域为结构强度、振动与可靠性

更新日期/Last Update: 2018-06-30