摘要
模拟小型燃气涡轮三盘非对称布置的转子 ,这种结构模型更接近于真实结构 ,但导致了理论分析的高度复杂性 ,推导了稳态动力响应的运动微分方程。
The differential equation system of motion for 3 discs asymmetrically arranged between two supports was developed for a modified small gas turbine in this paper.This model is somewhat close to a practical structure, but results in complication in theoretical analysis.
出处
《佛山科学技术学院学报(自然科学版)》
CAS
2001年第4期21-26,共6页
Journal of Foshan University(Natural Science Edition)
基金
国防预先研究课题资助项目 ( KT- 493)