Jet engine's speed controller with constant pressure chamber

被引:0
作者
Tudosie, Alexandru Nicolae [1 ]
机构
[1] Univ Craiova, Avion Dept, Fac Elect Engn, 105 Decebal Blvd, Craiova, Dolj, Romania
来源
PROCEEDINGS OF THE 9TH WSEAS INTERNATIONAL CONFERENCE ON AUTOMATION AND INFORMATION | 2008年
关键词
control; jet-engine; fuel injection; pressure chamber; actuator; fuel pump;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The paper deals with an automatic system meant to control a jet engine's rotation speed, through the fuel injection's control, based on a constant pressure chamber controller. One has established the non-linear mathematical model (based on the motion equations of the system's parts), the linear model and the nondimensional linear model, as well as the simplified model, the transfer function and the block-diagram. One had also performed a stability study and established the system's stability domains, as well as some quality studies.
引用
收藏
页码:560 / +
页数:2
相关论文
共 7 条
  • [1] Abraham R. H., 1986, COMPLEX DYNAMICAL SY
  • [2] Lungu R., 2000, FLIGHT APPARATUS AUT
  • [3] Mattingly J., 1996, ELEMENTS GAS TURBINE
  • [4] Stevens B.L., 1992, AIRCRAFT CONTROL SIM
  • [5] Stoenciu D., 1977, AIRCRAFT ENGINE AUTO
  • [6] Stoicescu M., 1999, TURBO JET ENGINES CH
  • [7] TUDOISE A, 2005, AEROSPACE PROPULSION