Abstract
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.
Original language | English |
---|---|
Pages (from-to) | 282-285 |
Number of pages | 4 |
Journal | Zhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosis |
Volume | 28 |
Issue number | 3 |
State | Published - Sep 2008 |
Keywords
- Data acquisition and processing
- Field balancing
- Micro turbo-jet engine
- Transient balancing