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:
Jul. 14, 2026

Filed:

Oct. 25, 2024
Applicant:

Verdego Aero, Inc., Daytona Beach, FL (US);

Inventors:

David N. Spitzer, Port Orange, FL (US);

Richard Pat Anderson, De Leon Springs, FL (US);

Patrick Currier, Port Orange, FL (US);

Austin Cassels, Daytona Beach, FL (US);

Assignee:

VerdeGo Aero, Inc., Daytona Beach, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/053 (2013.01);
Abstract

An aircraft powerplant includes an engine having an output power shaft. The aircraft powerplant further includes a power transmission coupled to the output power shaft of the engine. The power transmission is configured to divide power output of the engine between a mechanical power output and an electrical power output. A majority of the power output from the engine is adjustable to output to either of the mechanical power output or the electrical power output. The aircraft powerplant further includes a propulsion mechanism coupled to the mechanical power output. The aircraft powerplant further includes a control system configured to cause the power transmission to deliver the majority of the power output of the engine to the propulsion mechanism to generate thrust or deliver the majority of the power output of the engine as electrical power output via the electrical power output.


Find Patent Forward Citations

Spitzer, David. (2026). Hybrid turbofan engine with a planetary gearset for blending power between an electric output and variable-thrust bypass fan (U.S. Patent No. 12680508). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12680508

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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