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. 21, 2024

Filed:

Jul. 15, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Gary D. Roberge, Tolland, CT (US);

Jorn Axel Glahn, Manchester, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 5/08 (2006.01); F01D 25/12 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 5/085 (2013.01); F01D 25/125 (2013.01); F02K 3/06 (2013.01); F05D 2240/50 (2013.01); F05D 2240/55 (2013.01); F05D 2240/61 (2013.01); F05D 2260/20 (2013.01);
Abstract

A gas turbine engine includes a fan rotor, a compressor section, a combustor section, and a turbine section. The turbine section is positioned downstream of the combustor section. A fan drive turbine in the turbine section, and a shaft connects the fan drive turbine to the fan rotor. An inlet duct is connected to a cooling air source and connected to a cooling compressor downstream of the fan drive turbine. The cooling compressor is connected to an air source, and connected to a turning duct for passing compressed air in an upstream direction through the shaft. A method is also disclosed.


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