PDF下载 分享
[1]姚尚鹏,黄红,赵佳敏,等.涡轮泵典型故障仿真与辨识系统设计[J].火箭推进,2023,49(03):96-104.
 YAO Shangpeng,HUANG Hong,ZHAO Jiamin,et al.Typical fault simulation and identification system design for turbopump[J].Journal of Rocket Propulsion,2023,49(03):96-104.
点击复制

涡轮泵典型故障仿真与辨识系统设计

参考文献/References:

[1] 郑雄,杨勇,姚世东,等.法尔肯9可重复使用火箭发展综述[J].导弹与航天运载技术,2016(2):39-46.
[2] 康建斌,谢泽兵,郑宏涛,等.火箭子级垂直返回海上平台制导、导航和控制技术研究[J].导弹与航天运载技术,2016(6):32-35.
[3] JUE F,KUCK F.Space shuttle main engine(SSME)options for the future shuttle[C]//38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virginia:AIAA,2002.
[4] ZHANG Y L,WU J J,HUANG M C,et al.Liquid-propellant rocket engine health-monitoring techniques[J].Journal of Propulsion and Power,1998,14(5):657-663.
[5] MARKOU M,SINGH S.Novelty detection:A review.Part 1:statistical approaches[J].Signal Processing,2003,83(12):2481-2497.
[6] 张振臻,陈晖,高玉闪,等.液体火箭发动机故障诊断技术综述[J].推进技术,2022,43(6):20-38.
[7] 邓晨,薛薇,郑孟伟,等.大推力氢氧补燃循环发动机故障仿真[J].计算机测量与控制,2019,27(11):48-53.
[8] HONG T,LI H.Turbopump fault detection algorithm based on protruding frequency components RMS and SVM[C]//2013 IEEE International Conference on Mechatronics and Automation.New York:IEEE,2013.
[9] HU L,HU N Q,FAN B,et al.Application of novelty detection methods to health monitoring and typical fault diagnosis of a turbopump[J].Journal of Physics:Conference Series,2012,364:012128.
[10] ZHONG F L,LI H,WU Q,et al.A fault detection algorithm for turbopump based on lifting wavelet and LMS[C]//2013 IEEE International Conference on Mechatronics and Automation.New York:IEEE,2013.
[11] 张国渊,梁茂檀,郭进兴,等.不对中齿轮联轴器—轴承—转子系统动力特性[J].航空动力学报,2022,37(2):225-234.
[12] 金路,王俨剀,王彤,等.涡轮泵转子失稳故障分析[J].火箭推进,2020,46(4):23-30.
JIN L,WANG Y K,WANG T,et al.Analysis and diagnosis of turbine pump rotor instability[J].Journal of Rocket Propulsion,2020,46(4):23-30.
[13] JIANG P,XING Y Y,WANG B,et al.Reliability evaluation for turbo pump component in two-phase development with no failure data[C]//2019 Prognostics and System Health Management Conference.New York:IEEE,2019.
[14] VARTHA V,ARUN KUMAR M S,MATHEW S,et al.Failure analysis of ball-bearing of turbo-pump used in liquid rocket engine[J].Materials Science Forum,2015,830/831:709-712.
[15] AISWARYA N,SUJA PRIYADHARSINI S,MONI K S.An efficient approach for the diagnosis of faults in turbo pump of liquid rocket engine by employing FFT and time-domain features[J].Australian Journal of Mechanical Engineering,2018,16(3):163-172.
[16] 杨懿,陈文丽,王永鹏,等.基于Hilbert-Huang变换的液体火箭发动机涡轮泵故障分析[J].清华大学学报(自然科学版),2022,62(3):540-548.
[17] 杨硕.基于支持向量机的涡轮泵故障检测算法研究[D].成都:电子科技大学,2015.
[18] 夏鲁瑞,胡茑庆,秦国军.转速波动状态下涡轮泵典型故障诊断方法[J].推进技术,2009,30(3):342-346.
[19] 夏鲁瑞,胡茑庆,秦国军,等.涡轮泵启动过程振动故障检测方法[J].航空动力学报,2010,25(3):704-708.
[20] YIN Y C,LIU J F,WU X H,et al.An E-Bayesian estimation for reliability assessment of a success-failure type device[C]//2013 International Conference on Quality,Reliability,Risk,Maintenance,and Safety Engineering.New York:IEEE,2013.

相似文献/References:

[1]张晨曦,马晓丹.火箭发动机涡轮泵集成设计系统[J].火箭推进,2015,41(04):79.
 ZHANG Chenxi,MA Xiaodan.Integration design system for turbo pump in rocket engine[J].Journal of Rocket Propulsion,2015,41(03):79.
[2]李 彤,刘站国,窦 昱,等.涡轮泵水力试验系统扭矩现场校准技术研究[J].火箭推进,2015,41(03):73.
 LI Tong,LIU Zhan-guo,DOU Yu,et al.Field calibration technology for torque of turbo pump hydraulic test system[J].Journal of Rocket Propulsion,2015,41(03):73.
[3]窦 唯,刘占生.液体火箭发动机涡轮泵转子弯扭耦合振动研究[J].火箭推进,2012,38(04):17.
 DOU Wei,LIU Zhan-sheng.Research on bend-twist coupling vibration of liquid rocket engine turbopump rotors[J].Journal of Rocket Propulsion,2012,38(03):17.
[4]唐 飞,李家文.诱导轮平面叶栅汽蚀不稳定现象的数值分析[J].火箭推进,2011,37(01):34.
 TANG Fei,LI Jia-wen.Numerical analysis of instable cavitation phenomenon in 2D blade cascade of inducer[J].Journal of Rocket Propulsion,2011,37(03):34.
[5]白东安,段增斌,张翠儒.涡轮泵端面密封性能与漏气量影响研究[J].火箭推进,2010,36(01):38.
 Bai Dong'an,Duan Zenbin,Zhang Cuiru.Effects of leaking rate on turbopump end-face sealing performance[J].Journal of Rocket Propulsion,2010,36(03):38.
[6]邓长华,周云端.涡轮泵环形颗粒阻尼器设计[J].火箭推进,2009,35(05):29.
 Deng Changhua,Zhou Yunduan.Design of circular particle damper for turbopump[J].Journal of Rocket Propulsion,2009,35(03):29.
[7]白东安.涡轮泵超低工况性能研究[J].火箭推进,2008,34(03):13.
 Bai Dong'an.Research on the turbo-pump performance under ultra--low operation condition[J].Journal of Rocket Propulsion,2008,34(03):13.
[8]凌桂龙,张黎辉,唐家鹏,等.泵压式氢/氧液体火箭发动机质量分析[J].火箭推进,2007,33(01):1.
 Ling Guilong Zhang Lihui Tang Jiapeng.Mass analysis of pump-pressurized hydrogen/oxygen liquid propellant rocket engine[J].Journal of Rocket Propulsion,2007,33(03):1.
[9]黄智勇,李昌奂,黄红,等.高工况涡轮泵轴系状态对工作可靠性的影响[J].火箭推进,2007,33(01):32.
 Huang Zhiyong,Li Changhuan,Huang Hong.The effect of high operating condition turbopump shafting status on reliability[J].Journal of Rocket Propulsion,2007,33(03):32.
[10]徐悦,田爱梅.基于CFD的涡轮泵转子密封流体激振研究进展[J].火箭推进,2005,31(01):8.
 Xu Yue,Tian Aimei.Progress of investigation on turbopump annular seal fluid-induced vibration based on CFD[J].Journal of Rocket Propulsion,2005,31(03):8.

备注/Memo

收稿日期:2022-06-07; 修回日期:2022-07-11
基金项目:国家自然科学基金项目(12102348)
作者简介:姚尚鹏(1999—),男,硕士,研究领域为液体火箭发动机故障诊断及健康管理。

更新日期/Last Update: 1900-01-01