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:
Aug. 12, 2025

Filed:

Jan. 25, 2023
Applicant:

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

Inventor:

David Russell Trawick, Indianapolis, IN (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/024 (2025.01); B64D 35/023 (2025.01); F02C 6/00 (2006.01); F02C 7/36 (2006.01); H02K 7/00 (2006.01); H02K 7/102 (2006.01); H02K 7/116 (2006.01); H02K 7/14 (2006.01); H02K 7/18 (2006.01); H02K 11/00 (2016.01); H02P 1/54 (2006.01); H02P 3/04 (2006.01);
U.S. Cl.
CPC ...
B64D 35/024 (2024.01); B64D 35/023 (2024.01); F02C 6/00 (2013.01); F02C 7/36 (2013.01); H02K 7/006 (2013.01); H02K 7/102 (2013.01); H02K 7/116 (2013.01); H02K 7/14 (2013.01); H02K 7/1823 (2013.01); H02K 11/0094 (2013.01); H02P 1/54 (2013.01); F05D 2260/40311 (2013.01); H02P 3/04 (2013.01);
Abstract

An example aircraft includes a parallel propulsion unit, the parallel propulsion unit comprising: a propulsor configured to provide forward propulsion of the aircraft; a gas turbine engine configured to drive the propulsor; an electrical machine configured to generate, for output via one or more electrical busses, electrical energy using mechanical energy derived from the gas turbine engine; and a power sharing module configured to control a ratio of the mechanical energy used to drive the propulsor and used to generate electrical energy; and a plurality of series propulsion units, each series propulsion unit comprising a respective propulsor of a plurality of propulsors that are configured to provide vertical propulsion of the aircraft and a respective electrical machine of a plurality of electrical machines, each respective electrical machine configured to drive a respective propulsor of the plurality of propulsors using electrical energy received from one or more electrical busses.


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