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:
Jun. 30, 2026

Filed:

Jan. 09, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Neil Terwilliger, Meriden, CT (US);

Gary Collopy, Vernon, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/18 (2024.01); B64D 27/33 (2024.01); F01D 19/00 (2006.01); F02C 7/275 (2006.01); F02C 7/32 (2006.01);
U.S. Cl.
CPC ...
B64D 27/33 (2024.01); B64D 31/18 (2024.01); F01D 19/00 (2013.01); F02C 7/275 (2013.01); F02C 7/32 (2013.01); F05D 2270/023 (2013.01);
Abstract

A system includes a gas turbine engine of an aircraft, the gas turbine engine having a low speed spool, a high speed spool, and a combustor. The system also includes a low spool motor configured to augment rotational power of the low speed spool and a high spool motor configured to augment rotational power of the high speed spool. The system further includes a controller configured to cause fuel flow. The controller is configured to control a thrust response of the gas turbine engine to a thrust target between zero and a thrust level to move the aircraft during engine start and during engine idle. The controller is also configured to control the low spool motor to drive rotation of the low speed spool responsive to a thrust command while the controller does not command fuel flow to the combustor.


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