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. 10, 2023

Filed:

Dec. 31, 2019
Applicant:

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

Inventors:

William Anthony Amante, Grapevine, TX (US);

Karl Schroeder, Southlake, TX (US);

Joseph Richard Carpenter, Jr., Kennedale, TX (US);

Timothy Brian Carr, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); F16C 3/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 29/0091 (2013.01); F16C 3/02 (2013.01); F16C 2204/20 (2013.01); F16C 2226/60 (2013.01); F16C 2326/43 (2013.01);
Abstract

A ducted-rotor aircraft includes a fuselage, first and second ducts, and a spindle that is coupled to the fuselage. Each duct includes a rotor having a plurality of blades. The first and second ducts are coupled to opposed ends of the spindle. The spindle is rotatably coupled to the fuselage with first and second bearings. The first bearing is configured to react to radial loads and the second bearing is configured to react to both radial and axial loads. The spindle includes a shaft, first and second fittings secured to opposed ends of the shaft, and first and second attachment interfaces that are attachable to the first and second ducts. The attachment interfaces may be integral with the fittings. Alternatively, the fittings may be configured to be secured to the attachment interfaces with fasteners.


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