31th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion

ADAPTTIVE GTE SURGE PROTECTION SYSTEM WITH SELECTIVE CONTROL OF ACTUATORS

L.G. Bliznyukov¹, M.G. Kesselman¹, V.I. Chernyshov¹, S.A. Smetanin¹; ¹Central Institute of Aviation Motors, Russia

It describes new principles of surge protection system design, such as adaptation to compressor instability type (surge, rotating stall) during a flight and selective control of the actuators providing high-effective protection for various types of input effects and reducing total impulse loss.


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