Performance seeking control of turbo shaft engine with variable inlet guide vanes
|更新时间:2026-07-07
|
Performance seeking control of turbo shaft engine with variable inlet guide vanes
Vol. 26, Issue 10, (2011)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国航空工业集团公司 中国航空动力机械研究所,湖南,株洲,412002
3. 西北工业大学 动力与能源学院,西安,710072
作者简介:
基金信息:
DOI:
CLC:
Published:2011
稿件说明:
移动端阅览
ZHOU Jian-bo, SHI Rui-jun, ZHANG Qiu-gui, et al. Performance seeking control of turbo shaft engine with variable inlet guide vanes[J]. 2011, 26(10).
DOI:
ZHOU Jian-bo, SHI Rui-jun, ZHANG Qiu-gui, et al. Performance seeking control of turbo shaft engine with variable inlet guide vanes[J]. 2011, 26(10).DOI:
Performance seeking control of turbo shaft engine with variable inlet guide vanes
A mathematical model of turbo shaft engine with variable inlet guide vanes was established according to the theory of variable specific heat.Numerical simulations had been conducted on the mathematical model.The performance seeking control(PCS) modes of variable geometry turbo shaft engine had been investigated.Simulation results show that the engine model works well with higher accuracy and the PSC control modes can significantly improve the performance of turbo shaft engine.