An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.
COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS
2019-04-18
Patent
Electronic Resource
English
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