航天推进技术研究院主办
[1]金路,李爱民,陈晖,等.配合间隙对涡轮泵转子低速动平衡的影响研究[J].火箭推进,2017,43(04):14-17.
JIN Lu,LI Aimin,CHEN Hui,et al.Effect of tolerance clearance on low-speed dynamic balance of turbopump rotor[J].Journal of Rocket Propulsion,2017,43(04):14-17.
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JIN Lu,LI Aimin,CHEN Hui,et al.Effect of tolerance clearance on low-speed dynamic balance of turbopump rotor[J].Journal of Rocket Propulsion,2017,43(04):14-17.
配合间隙对涡轮泵转子低速动平衡的影响研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
43
期数:
2017年04期
页码:
14-17
栏目:
研究与设计
出版日期:
2017-10-01
- Title:
- Effect of tolerance clearance on low-speed dynamic balance of turbopump rotor
- Keywords:
- tolerance clearance; turbopump; rigid rotor; dynamic balance
- 分类号:
- TH113.1-34
- 文献标志码:
- A
- 摘要:
- 刚性涡轮泵转子低速动平衡是装配过程中的重要环节，残余不平衡量的大小是转子振动的关键影响因素之一，也是影响涡轮泵可靠性的重要因素。在某型发动机涡轮泵研制过程中，出现试车分解后不平衡量较装配时增加10～20倍的情况。对该涡轮泵转子建立了装配间隙对动平衡影响程度的理论模型，研究了不同零件的偏心距以及配合间隙对转子残余不平衡量的影响程度。根据影响程度对比，可以确定需要严格控制装配状态和单独动平衡的零件。通过反复拆装动平衡测试试验，对理论模型进行了验证。
- Abstract:
- Low-speed dynamic balance of rigid rotor is a very important link in the process of turbopump assemble. Residual imbalance is one of the key influence factor of rotor vibration, as well as an important factor affecting the reliability of turbopump. During the development of turbopump in a certain engine, the amount of imbalance after hot test was 10~20 times higher than that appeared in assemble process. The theoretical model of the turbopump rotor was established to determine the effect of the tolerance clearance on dynamic balance. The influence of mass eccentricity and tolerance clearance on the residual imbalance was studied. Those components whose assemble accuracy and balance need to be independently strengthened were determined by comparing the influence level. The dynamic balance experiments were done several times for validation of the theoretical model.
参考文献/References:
[1] 廖明夫. 航空发动机转子动力学[M]. 西安: 西北工业大
学出版社, 2015, 19-23.
[2] 王魁. 涡轮泵转子动平衡的控制方法研究[J]. 火箭推进,
2002, 28(6): 15-18.
WANG Kui. Study on control methool of turbopump roter
dynamic balance[J]. Journal of rocket propulsion. 2002, 28
(6): 15-18.
[3] 黄志勇, 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, 33(1): 32-35.
HUANG Zhiyong, LI Changhuan, HUANG Hong. The
effect of high operating condition turbopump shafting
status on reliability[J]. Journal of rocket propulsion, 2007,
33(1): 32-35.
[4] 窦唯, 叶志明, 闫宇龙. 涡轮泵叶轮/ 转子配合间隙对稳
定性的影响[J]. 火箭推进, 2016, 42(4): 26-34.
DOU Wei, YE Zhiming, YAN Yulong. Effect of tolerance
clearance between turbine rotor and impeller in
liquid-propellant rocket engine on stability[J]. Journal of
rocket propulsion, 2016, 42(4): 26-34.
[5] 李斌, 张贵田. 液体火箭发动机涡轮泵转子的新型动平
衡方法研究[J]. 振动与冲击, 2011, 30(6): 158-161.
[6] GB/T9239.1-2006. 机械振动恒态（刚性）转子平衡品质
要求[S].
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备注/Memo
收稿日期：2017-02-14；修回日期：2017-03-16 作者简介：金路（1986—），男，博士，研究领域为涡轮泵设计、转子动力学
更新日期/Last Update:
1900-01-01