FIELD: engines and pumps.
SUBSTANCE: tune-up method of gas turbine engine with augmentor involves fuel flow increase by influencing the fuel flow to augmentor, and control of change in dimensions of open flow area of jet nozzle in augmentor operating mode of the engine. When passage area reaches maximum value, tune-up is stopped.
EFFECT: reaching maximum thrust value in augmentor mode.
3 dwg
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