logo

For the Inventor, By the Inventor

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.

Patent No.:

US 12304624 B1

PDFFull Text
Date of Patent:
May. 20, 2025

Filed:

Jul. 10, 2023

Hybrid aircraft and landing launch/recovery system

Applicant:

Leigh Aerosystems Corporation, Vista, CA (US);

Inventors:

Gordon L. Harris, Vista, CA (US);

Stephen L. Harris, Vista, CA (US);

Assignee:

Leigh Aerosystems Corporation, Vista, CA (US);

Attorney:

Mintz Levin Cohn Ferris Glovsky and Popeo, P.C.

Primary Examiner:

Tye William Abell

Int. Cl.
CPC ...
B64U 10/20 (2023.01); B64C 3/56 (2006.01); B64C 27/26 (2006.01); B64D 27/02 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64U 70/93 (2023.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 3/56 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 27/026 (2024.01); B64U 10/20 (2023.01); B64U 70/93 (2023.01);
Abstract

An aircraft includes a fuselage extending along a first x-axis and a wing assembly including a first wing an a second wing. A first power assembly of the aircraft includes a first propulsion element and a first electric motor while a second power assembly includes a second propulsion element and a second electric motor. The aircraft further includes a third power assembly positioned aft of the first power assembly and the second power assembly. The third power assembly includes a third propulsion element and an internal combustion engine.

Find Patent Forward Citations

Quick Actions:

Harris, Gordon. (2025). Hybrid aircraft and landing launch/recovery system (U.S. Patent No. 12304624). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12304624

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

Loading…