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US Patent 11279479 Fluidic yaw control systems for use in hover

Patent 11279479 was granted and assigned to Textron on March, 2022 by the United States Patent and Trademark Office.

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Is a
Patent
Patent

Patent attributes

Patent Applicant
Textron
Textron
Current Assignee
Textron
Textron
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11279479
Date of Patent
March 22, 2022
Patent Application Number
16833638
Date Filed
March 29, 2020
Patent Citations
‌
US Patent 10384776 Tiltrotor aircraft having vertical lift and hover augmentation
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US Patent 10907669 Methods and apparatus for controlling flow fields
Patent Primary Examiner
‌
Assres H Woldemaryam
CPC Code
‌
B64C 21/04
‌
B64C 29/00
‌
B64C 39/10
‌
B64C 21/08

An active flow control system for generating yaw control moments for an aircraft during hover flight. The system includes right and left yaw effectors disposed proximate the right and left wingtips of the wing. A pressurized air system includes a pressurized air source and a plurality of injectors operably associated with the right and left yaw effectors. Based upon which of the injectors is injecting pressurized air, the right and left yaw effectors generate no yaw control moment, generate a yaw right control moment or generate a yaw left control moment.

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