航天推进技术研究院主办
DOU Wei,YAN Yu-long,JIN Zhi-lei,et al.Fatigue experiment of turbo-pump rotor at over-speed and high temperature condition[J].Journal of Rocket Propulsion,2015,41(01):15-22.
某发动机涡轮泵转子高温超速/疲劳试验研究
- Title:
- Fatigue experiment of turbo-pump rotor at over-speed and high temperature condition
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 涡轮转子是输送液氢/液氧推进剂的关键组件,其运行状态的好坏将直接影响发动机的性能和可靠性。超速/疲劳试验是转子质量控制、极限强度考核的一种试验方法。针对某发动机涡轮转子开展了高温超速/疲劳试验研究,首先研究了试验用转接器的设计方法,然后基于有限元方法建立了某液体火箭发动机涡轮泵转子高温超速试验的有限元模型,研究了温度对涡轮泵转子振型及临界转速等动特性的影响,分析了转子启动升速过程中常温和高温的振动幅值与支撑应力变化规律。在理论研究基础上开展了转子高温超速/疲劳试验研究,分析了高温状态下涡轮泵转子系统启动升速过程振动幅值的变化规律,研究了温度对涡轮泵转子超速动特性的影响规律。
- Abstract:
- In order to study the dynamic characteristics of turbo-pump rotor system in liquid- propellant rocket engine at high speed and high temperature condition, a finite element model for high temperature and over-speed test of turbo-pump rotor system in a liquid-propellant rocket engine was built by means of the finite element method to research the influence of temperature and critical speed on mode shape and dynamic characteristics of turbo-pump rotor system. The vibration state and bearing stress change rule in the startup process of rotor system in normal and high temperature are analyzed. The fatigue experiment of turbo-pump rotor in over-speed and high temperature was carried out. Based on simulation analysis, the influence rules of high temperature on the dynamic characteristics of turbo-pump rotor system have been mastered. The research result provided a basis for further research on dynamic performance of turbo-pump rotor system at high temperature.
参考文献/References:
[1]吴荣仁, 陆君毅. 飞轮的超速和飞裂试验研究[J]. 机电工程, 1993 (4): 28-30.
[2]窦唯, 褚宝鑫. 支承总刚度对泵转子临界转速及稳定性影响[J]. 火箭推进, 2014, 40(1): 30-38
[3]高兴, 黄科, 段浩. 高速叶轮的塑性变形特性分析[J], 鱼雷技术, 2013 (1): 14-19.
[4]BATHE K J. Finite element procedures in engineering analysis[M]. Englewood Cliffs, NJ: Prentice-Hall, 1982.
[5]钟一谔. 转子动力学[M]. 北京: 清华大学出版社, 1987.
[6]WU Jia-jang. Prediction of lateral vibration characteristics of a full-size rotor-bearing [J]. Finite Elements in Analysis and Design, 2007 (43): 803-816.
[7]窦唯. 液体火箭发动机涡轮泵转子密封系统动力稳定性研究[J]. 宇航学报, 2013, 34(12): 1557-1568.
[8]NELSON H D, MCVAUGH J M. The dynamics of rotor- bearing systems using finite elements[J]. Journal of En- gineering for Industry, 1976, 98 (2): 593-600.
[9]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(4): 17-25.
[10]郭维, 白东安. 液体火箭发动机用超低比转速离心泵优化设计[J]. 火箭推进, 2011, 37(5): 21-25.
[11]黄智勇, 李昌奂, 黄红. 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, 32(1): 32-35.
[12]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(1): 38-42.
相似文献/References:
[1]郑 伟,李护林,陈新红.激光快速成形技术在液体动力领域的应用前景[J].火箭推进,2015,41(06):1.
ZHENG Wei,LI Hulin,CHEN Xinhong.Application prospect of laser rapid prototyping
technology in the field of liquid power[J].Journal of Rocket Propulsion,2015,41(01):1.
[2]郭 敬,宋晶晶,孔凡超.发动机推进剂增压输送系统建模仿真技术综述[J].火箭推进,2015,41(05):1.
GUO Jing,SONG Jingjing,KONG Fanchao.Overview of modeling and simulation technology
for propellant pressurization feed system
of liquid rocket engine[J].Journal of Rocket Propulsion,2015,41(01):1.
[3]于 康,谢荣华,陈晓江.表面张力贮箱电子束焊接工艺研究[J].火箭推进,2015,41(05):89.
YU Kang,XIE Ronghua,CHEN Xiaojiang.Study on electron beam welding process
for surface tension tank[J].Journal of Rocket Propulsion,2015,41(01):89.
[4]刘中华,苏 晨,汪军安,等.气路膜片设计研究[J].火箭推进,2015,41(05):95.
LIU Zhonghua,SU Chen,WANG Junan,et al.Design and study of pneumatic diaphragm in gas circuit[J].Journal of Rocket Propulsion,2015,41(01):95.
[5]薛 薇,蔡震宇,曹红娟,等.基于可视化平台的液氢/液氧火箭发动机核心部件质量计算[J].火箭推进,2015,41(04):61.
XUE wei,CAI Zhenyu,CAO Hongjuan,et al.Mass calculation of key assembly units in
LH2/ LOX rocket engine based on visual interface[J].Journal of Rocket Propulsion,2015,41(01):61.
[6]穆朋刚,童 飞,蒲光荣,等.温度对贮箱增压系统的影响分析[J].火箭推进,2015,41(04):74.
MU Penggang,TONG Fei,PU Guangrong,et al.Influence of temperature on tank pressurization system[J].Journal of Rocket Propulsion,2015,41(01):74.
[7]高朝辉,刘 宇,肖 肖,等.垂直着陆重复使用运载火箭对动力技术的挑战[J].火箭推进,2015,41(03):1.
GAO Zhao-hui,LIU Yu,et al.Challenge to propulsion technology for vertical
landing reusable launch vehicle[J].Journal of Rocket Propulsion,2015,41(01):1.
[8]申智帅,等.气动增压器技术及其在空间推进系统的应用[J].火箭推进,2015,41(03):15.
SHEN Zhi-shuai,RUAN Hai-jun,et al.Pneumopump technology and its application
in space propulsion system[J].Journal of Rocket Propulsion,2015,41(01):15.
[9]张 翔,徐洪平,安雪岩,等.液体火箭发动机稳态运行故障
数据聚类分析研究0[J].火箭推进,2015,41(02):118.
ZHANG Xiang,XU Hong-ping,AN Xue-yan,et al.Clustering analysis for fault data in steady process of
liquid propellant rocket engine[J].Journal of Rocket Propulsion,2015,41(01):118.
[10]李 莹,潘宏亮,秦 飞,等.基于EASY5的液发系统建模与仿真可行性研究[J].火箭推进,2015,41(01):70.
LI Ying,PAN Hong-liang,QIN Fei,et al.Feasibility study on EASY5-based modeling and
simulation of liquid rocket engine[J].Journal of Rocket Propulsion,2015,41(01):70.
备注/Memo
收稿日期:2014-08-10;修回日期:2014-12-11 基金项目:中国航天科技集团公司重大工艺课题研究(ZDGY2013-35) 作者简介:窦唯(1977—),男,博士,高级工程师,研究领域为转子动力学及设备故障诊断技术研究