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:
Aug. 25, 2020

Filed:

Oct. 29, 2018
Applicant:

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

Inventors:

Andrew Paul Haldeman, Fort Worth, TX (US);

Zachary Edwin Dailey, Grapevine, TX (US);

Aaron Alexander Acee, Flower Mound, TX (US);

Dalton T. Hampton, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/605 (2006.01); B64C 27/06 (2006.01); B64C 27/00 (2006.01); B64C 13/04 (2006.01); B64C 13/40 (2006.01); B64C 27/72 (2006.01);
U.S. Cl.
CPC ...
B64C 27/605 (2013.01); B64C 13/0421 (2018.01); B64C 13/40 (2013.01); B64C 27/001 (2013.01); B64C 27/06 (2013.01); B64C 27/72 (2013.01); B64C 2027/004 (2013.01); B64C 2027/7216 (2013.01);
Abstract

An exemplary rotorcraft includes a power train with an engine coupled to a gearbox, a main rotor blade having a mast coupled to the power train, a control input linkage in communication between a pilot input device and the main rotor blade configured to communicate a control input force from the pilot input device to the main rotor blade, and a counterweight system in connection with the control input linkage and the power train to apply a centrifugal force to the control input linkage.


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