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:
Jun. 11, 2019

Filed:

Sep. 19, 2017
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Christopher M. Bothwell, Grapevine, TX (US);

Robert Earl Worsham, II, Weatherford, TX (US);

Sung Kyun Kim, Bedford, TX (US);

Brandon Jeffrey Thomas, Crowley, TX (US);

Assignee:

BELL HELICOPTER TEXTRON INC., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 27/82 (2006.01); B64D 43/00 (2006.01); B64C 13/04 (2006.01); B64C 13/50 (2006.01);
U.S. Cl.
CPC ...
B64D 45/0005 (2013.01); B64C 27/82 (2013.01); B64D 43/00 (2013.01); B64C 13/0421 (2018.01); B64C 13/503 (2013.01);
Abstract

In an embodiment, a rotorcraft includes: tail rotor blades; a tail rotor actuator coupled to the tail rotor blades such that the pitch of the tail rotor blades varies according to a current extension of the tail rotor actuator; pilot flight controls electrically coupled to the tail rotor actuator; and a flight control computer electrically coupled to the tail rotor actuator and the pilot flight controls, the flight control computer configured to: determine the current extension of the tail rotor actuator; determine whether the current extension of the tail rotor actuator is within a margin of a maximum extension of the tail rotor actuator; and indicate a first warning to a pilot in response to the current extension of the tail rotor actuator being within the margin of the maximum extension of the tail rotor actuator.


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