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:
Oct. 20, 2026

Filed:

Oct. 01, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Jeffrey T. Morton, Manchester, CT (US);

Melissa Coombes, Orono, ME (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); B64D 27/10 (2006.01); B64D 35/02 (2006.01); F02C 3/067 (2006.01); F02C 3/107 (2006.01); F02C 7/04 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64D 27/10 (2013.01); B64D 35/02 (2013.01); F02C 3/067 (2013.01); F02C 3/107 (2013.01); F02C 7/04 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2260/4031 (2013.01);
Abstract

An open propulsor rotor is configured to rotate about a first axis. An open guide vane structure includes a plurality of open guide vanes arranged circumferentially about a second axis offset from the first axis. The open guide vanes include a first open guide vane. A turbine engine includes a flowpath, a compressor section, a combustor section, a turbine section and a rotating assembly. The flowpath extends through the compressor section, the combustor section and the turbine section from an airflow inlet into the flowpath to a combustion products exhaust from the flowpath. The airflow inlet is axially aligned with or located forward of the first open guide vane along the second axis. The rotating assembly includes a turbine rotor disposed in the turbine section. The rotating assembly is configured to drive rotation of the open propulsor rotor through an offset geartrain.


Find Patent Forward Citations

Morton, Jeffrey. (2026). Open rotor aircraft propulsion system with offset geartrain (U.S. Patent No. 12767343). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12767343

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

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