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:
Sep. 15, 2026

Filed:

Jun. 26, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

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

Martin Amari, Glastonbury, CT (US);

Ninad Joshi, Brampton, CA;

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/12 (2006.01); B64C 15/02 (2006.01); B64D 27/16 (2006.01); B64D 27/33 (2024.01); B64D 31/18 (2024.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/12 (2013.01); B64C 15/02 (2013.01); B64D 27/16 (2013.01); B64D 27/33 (2024.01); B64D 31/18 (2024.01); B64D 27/026 (2024.01);
Abstract

An aircraft hybrid electrical propulsion (HEP) propulsion and attitude control system includes a propulsion system, electrical system and HEP controller. The propulsion system includes at least one propulsor and at least one electric motor configured to drive the at least one propulsor to generate to generate one or both of thrust and lift. The electrical system delivers a first amount of power to the at least one electric motor and a second amount of power to a plurality of electrical loads. The HEP controller determines at least one attitude goal of the aircraft, and controls the electrical system to adjust at least one of the thrust or lift to achieve the at least one attitude goal.


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