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:
Dec. 14, 2021

Filed:

Sep. 26, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Alan H. Epstein, Lexington, MA (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/275 (2006.01); B64D 27/10 (2006.01); B64D 31/02 (2006.01); B64D 33/08 (2006.01); F02C 7/12 (2006.01); F02C 7/27 (2006.01); F01D 25/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/275 (2013.01); B64D 27/10 (2013.01); B64D 31/02 (2013.01); B64D 33/08 (2013.01); F01D 25/36 (2013.01); F02C 7/12 (2013.01); F02C 7/27 (2013.01); F05D 2260/221 (2013.01); F05D 2260/85 (2013.01); F05D 2270/13 (2013.01);
Abstract

An engine system for an aircraft includes a first gas turbine engine, a first core turning system, a second gas turbine engine, and a second core turning system. The engine system also includes a controller operable to shutdown the first gas turbine engine responsive to determining that the aircraft has landed and operate in the second gas turbine engine in a taxi mode while using the first core turning system to cool the first gas turbine engine. The controller is further operable to shutdown the second gas turbine engine and disable the first core turning system based on a power-down condition, restart the first gas turbine engine and use the second core turning system to cool the second gas turbine engine based on a restart condition, and complete cooling of the second gas turbine prior to restarting the second gas turbine engine.


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