Composite airspeed indicator display for compound aircrafts
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United States of America Patent
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Jun 23, 2020
Grant Date -
Apr 18, 2019
app pub date -
Feb 8, 2018
filing date -
Oct 17, 2017
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Abstract
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.
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