PROPELLER-DRIVEN AIRCRAFT WITH ENGINE POWER SCHEDULING WITH INDICATED AIRSPEED

摘要

Propeller-driven aircraft (30) comprising an engine (31) providing mechanica l engine power for rotating a propeller (32), an engine limiting unit (35), an engine control unit (37) for controlling the mechanical engine power of the engine (31), a system (36) for measuring the airspeed and providing information concerning the airspeed to the engine limiting unit (35), wherei n the engine limiting unit (35) automatically reduces the mechanical engine power at airspeeds below a certain first airspeed value (V1).