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:
Jun. 23, 2026

Filed:

Jul. 18, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

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

Andrew E. Breault, Bolton, CT (US);

Roger Gates, West Hartford, CT (US);

Assignee:

RTX Corporation, Farmington, CT (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 2220/325 (2013.01); F05D 2260/40311 (2013.01);
Abstract

An assembly is provided for an aircraft. This assembly includes an open propulsor rotor, an engine core and a geartrain. The open propulsor rotor is configured to rotate about an axis. The engine core includes a flowpath, a compressor section, a combustor section, a turbine section and a rotating structure. The flowpath extends through the compressor section, the combustor section and the turbine section from an inlet into the flowpath to an exhaust from the flowpath. The rotating structure includes a compressor rotor in the compressor section and a turbine rotor in the turbine section. The rotating structure is configured to rotate about the axis and drive rotation of the open propulsor rotor. The geartrain is disposed axially between and operatively couples the rotating structure and the open propulsor rotor. The geartrain includes a star gear system and a planetary gear system.


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