Fluidic roll control systems for use in forward flight
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United States of America Patent
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Nov 16, 2021
Grant Date -
N/A
app pub date -
Mar 29, 2020
filing date -
Mar 28, 2020
priority date (Note) -
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Abstract
An active flow control system for generating roll control moments for an aircraft during forward flight. The system includes right and left roll effectors disposed on a trailing edge of the wing. A pressurized air system includes a pressurized air source and a plurality of injectors operably associated with the right and left roll effectors that influence the path of airflow across the wing. Based upon which of the injectors is injecting pressurized air, the right and left roll effectors generate no roll control moment, generate a roll right control moment or generate a roll left control moment.
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