DocumentCode :
1661331
Title :
LV100 gas turbine control: a case study
Author :
Ravi, R. ; Minto, K.D.
Author_Institution :
Control Syst. & Electron. Technol. Lab., Gen. Electr. Corp. Res. & Dev., Schenectady, NY, USA
Volume :
2
fYear :
1994
Firstpage :
1598
Abstract :
The subject of this case study is the LV100, a relatively new turbine engine targeted at land-based applications, specifically as the main propulsion unit in the next generation of armored vehicles. Because of its ground-based applications, the turbine is designed to run efficiently over a much larger range of operating points (speeds) than a corresponding aircraft engine would. A key element contributing to the success of the machine is the control system. While the present designs are within specifications, they are quite complicated. The focus of this study, therefore, is to bring to bear modern control design techniques to improving the control system. The paper describes in general terms the problem and the design specifications
Keywords :
control system analysis; control system synthesis; gas turbines; military equipment; propulsion; LV100 gas turbine control; armored vehicles; control system; design specifications; land-based applications; main propulsion unit; modern control design techniques; Computer aided software engineering; Control systems; Degradation; Engines; Process design; Shafts; Temperature control; Time factors; Turbines; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
Conference_Location :
Lake Buena Vista, FL
Print_ISBN :
0-7803-1968-0
Type :
conf
DOI :
10.1109/CDC.1994.411214
Filename :
411214
Link To Document :
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