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:
Apr. 19, 2022

Filed:

Nov. 26, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

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

Ramesh Rajagopalan, Glastonbury, CT (US);

Subhradeep Chowdhury, Rocky Hill, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02C 9/42 (2006.01); F02C 9/28 (2006.01);
U.S. Cl.
CPC ...
F02C 6/08 (2013.01); F02C 9/42 (2013.01); F02C 9/28 (2013.01); F05D 2260/96 (2013.01); F05D 2270/071 (2013.01);
Abstract

An engine system for an aircraft includes a first gas turbine engine, a second gas turbine engine, and a control system. The control system is configured to operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft and operate the second gas turbine engine with a sub-idle fuel burn schedule in the taxi mode of the aircraft. The sub-idle fuel burn schedule includes a reduction of the idle fuel burn schedule. A fuel flow of the first gas turbine engine and the second gas turbine engine is increased above the idle fuel burn schedule prior to takeoff of the aircraft.


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