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:
Apr. 08, 2025

Filed:

Jun. 14, 2019
Applicant:

The Texas A&m University System, College Station, TX (US);

Inventors:

Moble Benedict, College Station, TX (US);

David Coleman, Bryan, TX (US);

Atanu Halder, College Station, TX (US);

Bochan Lee, College Station, TX (US);

Andrew Riha, Bryan, TX (US);

Farid Saemi, Houston, TX (US);

Carl Runco, College Station, TX (US);

Vishaal Subramanian, College Station, TX (US);

Eric Greenwood, Newport News, VA (US);

Vinod Lakshminarayan, Sunnyvale, CA (US);

Assignee:

The Texas A&M University System, College Station, TX (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/68 (2006.01); B60L 15/20 (2006.01); B60L 50/60 (2019.01); B64C 27/10 (2023.01); B64C 27/467 (2006.01); B64C 27/605 (2006.01); B64D 17/80 (2006.01); B64D 27/24 (2024.01); B64D 31/00 (2024.01);
U.S. Cl.
CPC ...
B64C 27/68 (2013.01); B60L 15/20 (2013.01); B60L 50/60 (2019.02); B64C 27/10 (2013.01); B64C 27/467 (2013.01); B64C 27/605 (2013.01); B64D 17/80 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B60L 2200/10 (2013.01);
Abstract

A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades, a first actuation assembly including a first plurality of electronically controlled actuators coupled to a first swashplate and configured to control the movement of the first swashplate relative to the body, and a control system coupled to the body and configured to control the first plurality of actuators, wherein the control system includes a cable extending through a passage formed in the tubular strut and in signal communication with the first plurality of actuators.


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