FIELD: power engineering.
SUBSTANCE: invention relates to power engineering. The method to regulate surging for a gas turbine engine, including representation of a gas turbine engine, comprising a compressor, a combustion chamber, downstream the compressor, with a tract of hot gases, a turbine downstream the combustion chamber, with a tract of hot gases, besides, the outlet flow from the compressor is regulated, on the basis of control for the purposes of adjustment to exclude the surging condition, and direction of the outlet flow to at least one of tracts of hot gases to avoid at least some of the combustion chamber. Also a gas turbine engine is provided for realisation of the method according to the invention.
EFFECT: invention makes it possible for a gas turbine to operate with improved efficiency, and also makes it possible to actively prevent compressor surging.
13 cl, 2 dwg
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