Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Sog-Kyun Kim"'
Autor:
Sog-Kyun Kim, Peter J. Fleming, S. Regunath, Tim Breikin, I.D. Herbert, S. M. Hargrave, Haydn A. Thompson
Publikováno v:
Control Engineering Practice. 14:387-396
This paper discusses the findings of an analysis of an aero engine staged combustion fuel distribution control system design in the framework of the LECCAGT research project. The paper outlines the motivation for developing a staged combustion system
Publikováno v:
IFAC Proceedings Volumes. 35:265-270
This paper focuses on multi-objective optimisation of staged combustion control for aviation gas turbine engines. Pareto optimisation based multi-objective genetic algorithms are used to design the fuel distribution control laws of a staged combustor
Publikováno v:
Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs.
Real-Time Engine Models are required for operation with engine electronic control systems and/or aircraft simulators for functional demonstration. The challenge for Rolls-Royce has been to establish the sub-idle speed behaviour of the engine. This pa
Publikováno v:
Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs.
The developments of high bypass turbofan engines and improvements in high temperature materials have resulted in smaller engine cores. These smaller core engines result in correspondingly lower airflows that introduce their own design problems, inclu
Publikováno v:
Proceedings of 2003 IEEE Conference on Control Applications, 2003. CCA 2003..
Using gas turbine engine test data, a fuzzy model is obtained using cluster estimation and multi-objective optimisation. Cluster estimation provides the mechanism for calculating the density of the data distribution and for extracting useful informat
Publikováno v:
Volume 2: Turbo Expo 2004.
Surge margin tracking logic is developed for use in the control of quick windmill relighting (QWR) at sub-idle. Using existing high pressure compressor (HPC) characteristics (but without any gas turbine engine model), the surge margin can be calculat
Publikováno v:
SAE Technical Paper Series.
Autor:
Sog-Kyun Kim, C. D. Kong
Publikováno v:
ASME 1997 Turbo Asia Conference.
A combustor and a fuel nozzle for a small aircraft gas turbine were designed and appropriateness for design requirements were evaluated and confirmed through the cold and hot test. For the purpose of studying the flame stability of a pilot atomizer u
Publikováno v:
Proceedings of 2003 IEEE Conference on Control Applications, 2003 (CCA 2003); 2003, p564-564, 1p