An aircraft is provided and includes one or more main rotors, one or more and propellers including blades that are rotatable about a rotational axis, a pitch of each of the blades being controllable, and a flight control computer disposed to control the pitch of each of the blades to reduce propeller blade pitch angles in an event of an engine failure.
AUTOMATIC PROPELLER TORQUE PROTECTION SYSTEM
2016-03-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Engineering Index Backfile | 1919
|Digital propeller torque conversion control device and propeller torque conversion control system
Europäisches Patentamt | 2024
|