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:
May. 11, 2021

Filed:

Apr. 02, 2018
Applicant:

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

Inventors:

Tyler Wayne Baldwin, Keller, TX (US);

Michael Dearman, Weatherford, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/04 (2006.01); F16D 3/60 (2006.01); F16D 1/10 (2006.01); B64F 5/10 (2017.01); B64C 29/00 (2006.01); B29C 70/84 (2006.01); B29L 31/00 (2006.01); B22D 25/02 (2006.01); B29K 705/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/04 (2013.01); B64F 5/10 (2017.01); F16D 1/10 (2013.01); F16D 3/60 (2013.01); B22D 25/02 (2013.01); B29C 70/84 (2013.01); B29K 2705/00 (2013.01); B29L 2031/7498 (2013.01); B64C 29/0033 (2013.01); F16D 2001/103 (2013.01); Y10S 16/41 (2013.01); Y10S 464/904 (2013.01);
Abstract

A light weight hybrid torque transfer joint trunnion has an integral metal hub spline fitting oriented on a center axis. This integral metal hub spline fitting may be made of steel, aluminum, titanium, or the like and may be generally cylindrical. The integral metal hub spline fitting defines an integral central internally-splined mast or driveshaft coupling opening centered about the center axis. A composite material body centrally retains, and is cured to, the metal hub spline fitting. Torque transfer joint link attachment pins extend from the composite material body and are rigidly linked to the metal hub spline fitting. In an example constant-velocity joint, a plurality of pivoting linkages may each be rotatably coupled to the torque transfer joint link attachment pins, and each of the plurality of pivoting linkages may, in turn be secured to a rotor yoke configured to mount a plurality of rotorcraft blades.


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