Scaling limits of the thrust changed to control thrust asymmetry

摘要

Abstract invention patent: "scaling limits of the thrust changed to control thrust asymmetry.The present invention relates to a function of flight control and motor control for an aircraft multiple engines which automatically controls the maximum thrust engine in operation to a value lower than the scaling limits of nominal thrust in case of loss of thrust in another M Otor.The maximum engine thrust of engine operation is controlled (limited) in such a way that the asymmetry of the resulting thrust can be controlled at air speeds lower than would be the case in another way.The decrease in the minimum control speed with engine cut can reduce the limitation of landing speeds which would otherwise be caused by speed control motor minimum cut.