A torque indicator for an aircraft having a main rotor system and a translational thrust system driven by at least one engine includes a first indicator operable to display an actual torque of an engine of the aircraft relative to an engine torque limit, a second indicator operable to display an actual torque of the translational thrust system of the aircraft relative to a translational thrust system torque limit, and a third indicator operable to display an actual torque of the main rotor system of the aircraft relative to a main rotor system torque limit.
COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS
18.04.2019
Patent
Elektronische Ressource
Englisch
Composite airspeed indicator display for compound aircrafts
Europäisches Patentamt | 2020
|COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS
Europäisches Patentamt | 2019
|Composite airspeed indicator display for compound aircrafts
Europäisches Patentamt | 2020
|An alternative neural airspeed computation method for aircrafts
Emerald Group Publishing | 2018
|AIRSPEED INDICATOR (PITOT STATIC)
SAE Technical Papers | 1947