METHOD OF AIRCRAFT TURBOPROP CONTROL

摘要

FIELD: transport.SUBSTANCE: invention relates to aircraft engineering and may be used in aircraft turboprop ACS electronic and hydromechanical hardware. Proposed invention consists in additional control over mismatch between preset and measured angle of pitch of propeller. In case said mismatch exceeds preset magnitude determined by calculations and experiments duel consumption rate is corrected.EFFECT: higher reliability of ACS and aircraft safety.1 dwg