The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 31, 2023

Filed:

Jan. 19, 2021
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Albert G Brand, North Richland Hills, TX (US);

Bradley P. Regnier, Fort Worth, TX (US);

Matthew J. Hill, Keller, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/78 (2006.01); B64C 27/57 (2006.01); B64C 27/68 (2006.01); B64C 27/82 (2006.01); B64D 45/00 (2006.01); B64C 27/06 (2006.01);
U.S. Cl.
CPC ...
B64C 27/78 (2013.01); B64C 27/06 (2013.01); B64C 27/57 (2013.01); B64C 27/82 (2013.01); B64D 45/00 (2013.01); B64C 2027/8209 (2013.01);
Abstract

Embodiments are directed to a flight control system for a helicopter comprises a pilot interface configured to receive a control input, at least one electronically controlled actuator, and a computing device configured to translate the control input to an actuator command, wherein the computing device is further configured to apply yaw rate limits to the actuator command to avoid loss of tail rotor effectiveness. The yaw rate limits are associated with a vortex ring state (VRS) envelope for a tail rotor of the helicopter. The electronically controlled actuator comprises a tail rotor actuator. The control input is a pedal input.


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