This invention discloses a starting control method,
system, equipment, aircraft, and medium for a
propeller-driven aircraft
piston engine, relating to the field of aero-engine control technology. The method includes: performing a power-on self-test before starting, checking the minimum
propeller blade angle,
throttle opening, and fuel pressure; after the self-test, the flight control computer automatically and adaptively controls the starting
throttle opening and target starting speed based on altitude and atmospheric static temperature; during starting, status monitoring is performed,
towing the engine to a state capable of ignition and
fuel injection control; after successful starting, the lubricating
oil temperature is determined to automatically set the corresponding
throttle opening and warm-up speed; finally, a dual
ignition system check and pre-flight condition checks are performed. This invention achieves fully closed-loop
adaptive control, effectively overcoming starting difficulties in complex environments such as high altitudes and frigid conditions, eliminating the hidden dangers of starting with defects, and significantly improving the timeliness of the aircraft's maneuverability and
operational safety.