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:
Jan. 18, 2022

Filed:

Aug. 15, 2019
Applicant:

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

Inventors:

Keith Alan Stanney, Dallas, TX (US);

Steven Ray Ivans, Ponder, TX (US);

Brent Chadwick Ross, Flower Mound, TX (US);

Troy Bushmire, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/28 (2006.01); B64C 17/02 (2006.01); B64C 3/56 (2006.01); B64C 27/50 (2006.01); B64C 27/26 (2006.01); B64C 27/82 (2006.01); B64C 1/30 (2006.01);
U.S. Cl.
CPC ...
B64C 27/28 (2013.01); B64C 3/56 (2013.01); B64C 17/02 (2013.01); B64C 27/26 (2013.01); B64C 27/50 (2013.01); B64C 27/82 (2013.01); B64C 1/30 (2013.01); B64C 2027/8281 (2013.01);
Abstract

Embodiments are directed to a rotorcraft comprising a body having a longitudinal axis, a wing coupled to the body, a single tiltrotor assembly pivotally coupled to the body, and the tiltrotor assembly configured to move between a position generally perpendicular to the longitudinal axis during a vertical flight mode and a position generally parallel to the longitudinal axis during a horizontal flight mode. The rotorcraft may further comprise an anti-torque system configured to counteract torque generated by the tiltrotor assembly during vertical flight. The rotorcraft may further comprise a center of gravity compensation system configured to manage a rotorcraft center of gravity during movement of the tiltrotor assembly between the vertical flight mode and the horizontal flight mode.


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