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:
Dec. 30, 2025

Filed:

Dec. 19, 2024
Applicants:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

Robert W. Heeter, Indianapolis, IN (US);

Daniel E. Molnar, Jr., Indianapolis, IN (US);

Jordan Thralls, Indianapolis, IN (US);

Assignees:

Rolls-Royce North American Technologies, Inc., Indianapolis, IN (US);

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F02C 6/00 (2006.01); F02C 6/20 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F02C 6/00 (2013.01); F02C 6/20 (2013.01); H02K 7/1823 (2013.01);
Abstract

A turbine engine includes at least one turbine, combustion equipment, and at least one compressor. The at least one compressor includes a compressor stage. The compressor stage includes a plurality of compressor blades configured to input work into a core airflow flowing through the turbine engine. The turbine engine includes an electrical generator. The electrical generator includes a rotor carried on an outer diameter of the plurality of compressor blades of the compressor stage and mechanically rotated by the plurality of compressor blades of the compressor stage and configured to rotate about a longitudinal axis of the turbine engine. The electrical generator further includes a stator.


Find Patent Forward Citations

Loading…