CAJ | 학술논문

本文通过对甩负荷试验测试数据的计算与分析，考虑到甩负荷“0”时刻、调速器及定子铁心损耗的影响，对飞轮力矩进行了求取。得出在低负荷的试验工况下，常规甩负荷试验可以进行飞轮力矩测定的结论。并根据测试数据，确定了机组转动部分的飞轮力矩。
본문통과대솔부하시험측시수거적계산여분석，고필도솔부하“0”시각、조속기급정자철심손모적영향，대비륜력구진행료구취。득출재저부하적시험공황하，상규솔부하시험가이진행비륜력구측정적결론。병근거측시수거，학정료궤조전동부분적비륜력구。
The paper determines the flywheel moment with the load rejection test data. In consideration of the load rejection“0”moment, and the influence of governer as well as stator core losses. The conclusion can be achieved for measurement of flywheel moment at proper load rejection test under low load test condition. With the test data, a flywheel moment is determined.