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:
Oct. 26, 2021

Filed:

Oct. 04, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Lawrence Binek, Glastonbury, CT (US);

Jesse R. Boyer, Middletown, CT (US);

Om P. Sharma, South Windsor, CT (US);

Evan Butcher, Suffield, CT (US);

Bryan G. Dods, Greer, SC (US);

Vijay Narayan Jagdale, South Windsor, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F02K 3/10 (2006.01); B33Y 80/00 (2015.01); F23R 3/20 (2006.01); F02C 3/05 (2006.01); F02C 3/14 (2006.01); F23R 3/34 (2006.01); F23R 3/54 (2006.01);
U.S. Cl.
CPC ...
F02C 3/05 (2013.01); F02C 3/145 (2013.01); F02C 7/222 (2013.01); F02K 3/10 (2013.01); B33Y 80/00 (2014.12); F05D 2240/14 (2013.01); F05D 2240/35 (2013.01); F23R 3/20 (2013.01); F23R 3/346 (2013.01); F23R 3/54 (2013.01);
Abstract

A gas turbine engine is provided that includes a compressor section, a turbine section, and a unitary structure. The compressor section has at least one compressor rotor stage. The turbine section has at least one turbine rotor stage. The compressor rotor stage and the turbine rotor stage are in rotational communication with each other. The unitary structure includes an outer case portion, a combustor section, a turbine nozzle, and an exhaust duct. The unitary structure configured for attachment with the turbine section and compressor section.


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