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:
Mar. 25, 2025

Filed:

Jan. 11, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Stephen A. Witalis, Glastonbury, CT (US);

Ramesh Rajagopalan, Glastonbury, CT (US);

Manuj Dhingra, Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/00 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 31/06 (2006.01); F02C 7/26 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); F02C 6/00 (2013.01); F02C 7/26 (2013.01); B64D 27/026 (2024.01); F05D 2260/85 (2013.01);
Abstract

An engine system for an aircraft includes a gas turbine engine and a control system. The control system is configured to motor the gas turbine engine, absent fuel burn, during a taxi mode of the aircraft. The control system is further configured to accelerate a motoring speed of the gas turbine engine, absent fuel burn, above an idle speed of the gas turbine engine to provide propulsion during the taxi mode. The control system is configured to decrease the motoring speed of the gas turbine engine, absent fuel burn, based on a change in a starting mode of the gas turbine engine or the aircraft reaching a targeted new position.


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