FIELD: power engineering. SUBSTANCE: system has interconnected selector and mode setters. When engine runs with air taken from compressor for aircraft stabilization or control, setter passes signal to selector. Upon arrival of signal from setter selector shapes output signal supplied to input of logic element. If draft is to be increased when engine runs without taking air from compressor for aircraft stabilization and control, setter shapes signal passed to input of selector which simulates signal fed to input of logic element from sensor in proportion to position of air take-off cock from compressor when opened fully or partially. EFFECT: improved reliability of stabilization and control. 2 dwg
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