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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.

Patent No.:

US 12654670 B1

PDFFull Text
Date of Patent:
Jun. 16, 2026

Filed:

Mar. 06, 2023

Aircraft hybrid electric propulsion architecture enabling modes of operation

Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Zubair A. Baig, South Windsor, CT (US);

Martin Amari, Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:

CANTOR COLBURN LLP

Primary Examiner:

Phutthiwat Wongwian

Assistant Examiner:

Jacek undefined Lisowski

Int. Cl.
CPC ...
B64D 27/33 (2024.01); B60L 1/08 (2006.01); B60W 10/08 (2006.01); B64D 27/02 (2006.01); B64D 27/24 (2006.01); B64D 31/18 (2024.01); F01D 15/10 (2006.01); H02J 105/30 (2026.01); H02J 105/50 (2026.01); H02J 105/52 (2026.01); H02P 101/30 (2015.01);
U.S. Cl.
CPC ...
B60W 10/08 (2013.01); B60L 1/08 (2013.01); B64D 27/026 (2024.01); B64D 27/24 (2013.01); B64D 27/33 (2024.01); B64D 31/18 (2024.01); B64D 2221/00 (2013.01); F01D 15/10 (2013.01); F05D 2220/323 (2013.01); F05D 2270/05 (2013.01); H02J 2105/32 (2026.01); H02J 2105/51 (2026.01); H02J 2105/52 (2026.01); H02P 2101/30 (2015.01);
Abstract

An aircraft hybrid electrical propulsion (HEP) system includes an electrical system configured to deliver power to a plurality of electrical loads, a propulsion system configured to generate thrust in response to an input power, and an HEP controller in signal communication with the electrical system and the propulsion system. The HEP controller is configured to monitor a load demand of at least one electrical load among the plurality of electrical loads and to actively control the input power to actively control the thrust in response to changes in the load demand.

Find Patent Forward Citations

Baig, Zubair. (2026). Aircraft hybrid electric propulsion architecture enabling modes of operation (U.S. Patent No. 12654670). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12654670

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

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