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:
May. 06, 2025

Filed:

Oct. 24, 2022
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventor:

Martin Richard Amari, Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/00 (2005.12); B64D 27/10 (2005.12); B64D 27/24 (2005.12); B64D 31/12 (2005.12); F02C 7/00 (2005.12); F02C 9/42 (2005.12); G05D 1/00 (2005.12); B64D 27/02 (2005.12);
U.S. Cl.
CPC ...
F02C 6/00 (2012.12); B64D 27/10 (2012.12); B64D 27/24 (2012.12); B64D 31/12 (2012.12); F02C 7/00 (2012.12); F02C 9/42 (2012.12); G05D 1/101 (2012.12); B64D 27/026 (2023.12);
Abstract

A system of a hybrid aircraft includes a first gas turbine engine, a second gas turbine engine, and a controller. The first gas turbine engine includes a first low spool electric machine and a first high spool electric machine. The second gas turbine engine includes a second low spool electric machine and a second high spool electric machine. The controller is operable to determine an operating mode of the hybrid aircraft and control power extraction from either or both of the first low spool electric machine and the first high spool electric machine while a single engine descent mode is active. Electric power is provided to either or both of the second low spool electric machine and the second high spool electric machine while the single engine descent mode is active to balance thrust between the first gas turbine engine and the second gas turbine engine.


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