METHOD FOR CONTROLLING AN AIRCRAFT TURBOJET ENGINE Russian patent published in 2017 - IPC F02C9/00 

FIELD: airpower.

SUBSTANCE: method for controlling an aircraft turbojet engine, in which two or more programs for adjusting the installation angles of the compressor guiding devices are formed in addition in the working range of the installation angles of the compressor guide devices in advance for this type of engine, depending on its reduced speed. During the flight of the aircraft, when switching to the cruising mode of the engine operation, the switching signal of the compressor control units is switched on depending on the reduced speed of the program, which ensures the minimum fuel consumption in the given thrust range.

EFFECT: invention allows to increase the reliability of switching by the engine regulator to the control program of the compressor directing devices, which ensures a minimum fuel consumption in the given thrust range, during the transition to the cruising mode of the engine, and also allows to reduce fuel consumption in this mode.

2 dwg, 1 tbl