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. 23, 2022

Filed:

Nov. 08, 2019
Applicant:

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

Inventors:

George Matthew Thompson, Lewisville, TX (US);

Paul Sherrill, Grapevine, TX (US);

Jonathan Knoll, Burleson, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
A47C 7/74 (2006.01); B64D 35/04 (2006.01); B64C 11/00 (2006.01); B64C 11/46 (2006.01); B64D 27/24 (2006.01); B64C 29/00 (2006.01); F16H 57/02 (2012.01);
U.S. Cl.
CPC ...
B64D 35/04 (2013.01); B64C 11/001 (2013.01); B64C 11/46 (2013.01); B64D 27/24 (2013.01); B64C 29/0033 (2013.01); F16H 2057/02034 (2013.01); F16H 2057/02043 (2013.01);
Abstract

A rotor assembly including a rotor mast, a rotor hub coupled to the rotor mast, a plurality of rotor blades coupled to the rotor hub, a control tube extending through the rotor mast, a crosshead coupled to the control tube, and a mechanism configured to drive the rotor mast in rotation. Wherein the mechanism is longitudinally positioned between a top portion and a bottom portion of the control tube and translation of the control tube relative to the rotor mast causes rotation of the rotor blades about their pitch-change axes. While the crosshead is installed, the crosshead is prevented from angular rotation about the mast axis. A pin of a rotor blade assembly is captured between opposing tabs of the crosshead and movable relative to the opposing tabs in response to translation of the crosshead along the mast axis.


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