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An extrapolation approach for aeroengine's transient control law design 被引量:8

An extrapolation approach for aeroengine's transient control law design
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摘要 Transient control law ensures that the aeroengine transits to the command operating state rapidly and reliably. Most of the existing approaches for transient control law design have complicated principle and arithmetic. As a result, those approaches are not convenient for application. This paper proposes an extrapolation approach based on the set-point parameters to construct the transient control law, which has a good practicability. In this approach, the transient main fuel control law for acceleration and deceleration process is designed based on the main fuel flow on steady operating state. In order to analyze the designing feature of the extrapolation approach, the simulation results of several different transient control laws designed by the same approach are compared together. The analysis indicates that the aeroengine has a good performance in the transient process and the designing feature of the extrapolation approach conforms to the elements of the turbofan aeroengine. Transient control law ensures that the aeroengine transits to the command operating state rapidly and reliably. Most of the existing approaches for transient control law design have complicated principle and arithmetic. As a result, those approaches are not convenient for application. This paper proposes an extrapolation approach based on the set-point parameters to construct the transient control law, which has a good practicability. In this approach, the transient main fuel control law for acceleration and deceleration process is designed based on the main fuel flow on steady operating state. In order to analyze the designing feature of the extrapolation approach, the simulation results of several different transient control laws designed by the same approach are compared together. The analysis indicates that the aeroengine has a good performance in the transient process and the designing feature of the extrapolation approach conforms to the elements of the turbofan aeroengine.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第5期1106-1113,共8页 中国航空学报(英文版)
基金 support of Aeronautical Science Foundation of China (2011ZB51019)
关键词 Acceleration control law Acceleration and deceleration characteristic Aeroengine control Deceleration control law Extrapolation approach Transient control law Turbofan engine Acceleration control law Acceleration and deceleration characteristic Aeroengine control Deceleration control law Extrapolation approach Transient control law Turbofan engine
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