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:
Mar. 11, 2025

Filed:

Sep. 07, 2023
Applicant:

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

Inventors:

Kirk L. Groninga, Keller, TX (US);

Danielle L. Edwards, Grapevine, TX (US);

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/16 (2006.01); B64C 15/12 (2006.01); B64C 29/00 (2006.01); B64C 39/04 (2006.01);
U.S. Cl.
CPC ...
B64C 1/16 (2013.01); B64C 15/12 (2013.01); B64C 29/0033 (2013.01); B64C 39/04 (2013.01);
Abstract

A rotating pylon assembly for aircraft thrust vectoring control. In embodiments, the rotating pylon assembly of embodiments includes a rotating sleeve disposed within a fixed boom of the aircraft, and configured to support a rotor assembly. The rotating pylon assembly includes a bearing assembly configured to functionally couple the rotating sleeve against an inner surface of the fixed boom. The bearing assembly enables the rotating sleeve to rotate against the inner surface of the fixed boom and about a longitudinal axis of the fixed boom. An actuator is configured to rotate the rotating sleeve about the longitudinal axis of the fixed boom. The rotating sleeve may cause the rotor assembly to be rotated or swung about the longitudinal axis of the fixed boom to position the rotor assembly in a position to vector the thrust provided by the rotor assembly based on a control command.


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