摘要
Theories related to rotor transient balancing were discussed. The correction plane of field balancing for a micro turbo-jet engine was analyzed and determined. The way to build up a computer aided transient field balancing system and its operation principle were presented. By using the transient field balancing system, a model rotor was balanced, and the balancing precision obtained meets the requirements of international standards.
源语言 | 英语 |
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页(从-至) | 282-285 |
页数 | 4 |
期刊 | Zhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosis |
卷 | 28 |
期 | 3 |
出版状态 | 已出版 - 9月 2008 |