FIELD: engines.
SUBSTANCE: invention relates to method of elimination of rotating failure in compressor of gas turbine engine, which includes following stages: stage of automatic detection of stalling in gas turbine engine; stage of automatic shutdown of gas turbine engine; in case of detection stage of automatic recovery of surge reserve shift; stage of automatic repeated ignition of gas turbine engine.
EFFECT: high-effective elimination of rotating failure.
9 cl, 3 dwg
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