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. 15, 2025

Filed:

Nov. 04, 2024
Applicants:

General Electric Company, Evendale, OH (US);

GE Avio S.r.l., Rivalta di Torino, IT;

Inventors:

Arthur W. Sibbach, Boxford, MA (US);

Vincenzo Martina, Rivalta di Torino, IT;

Tomasz Iglewski, Warsaw, PL;

Assignees:

General Electric Company, Evendale, OH (US);

GE Avio S.r.l., Rivalta di Torino, IT;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); B64D 27/33 (2024.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64D 27/33 (2024.01); B64D 2033/0293 (2013.01);
Abstract

A hybrid electric turboprop includes a propeller, a thermal engine, an electric motor, a gearbox, and an air inlet. The propeller is configured to rotate about a propeller axis and includes a plurality of blades extending radially outwardly from the propeller axis such that, as the propeller is rotated about the propeller axis, the plurality of blades define a substantially circular blade path area centered about the propeller axis and having a radius. The gearbox couples both the thermal engine and the electric motor to the propeller to enable each of the thermal engine and the electric motor to drive rotation of the propeller about the propeller axis. The air inlet defines an opening. A radial distance is defined from the propeller axis to a location within the opening. The radial distance is equal to or less than 60% of the radius.


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