An engine and propeller control system (EPECS) of an aircraft includes a propeller (30) with a plurality of blades (110) coupled to an aircraft engine. Each of the blades (110) are coupled to an actuator (111) configured to adjust the blades (110) between a first pitch to produce forward thrust and a second pitch to produce reverse thrust. The EPECS (200) further includes a controller (250) configured to control the actuator (111) to invoke the second pitch in response to receiving a reverse thrust command signal. The controller (250) is configured to alert that the reverse thrust command signal is generated prior to landing the aircraft.
DISENGAGEMENT FOR REVERSE PROPELLER PROTECTION
ABKOPPLUNG FÜR UMKEHRPROPELLERSCHUTZ
DÉBRAYAGE POUR LA PROTECTION CONTRE L'HÉLICE INVERSÉE
18.06.2025
Patent
Elektronische Ressource
Englisch
Tema Archiv | 2007
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