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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.

Patent No.:

US 11156156 B1

PDFFull Text
Date of Patent:
Oct. 26, 2021

Filed:

Oct. 04, 2018

Gas turbine engine with a unitary structure and method for manufacturing the same

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:

Getz Balich LLC

Primary Examiner:

Gerald L Sung

Assistant Examiner:

Stephanie Sebasco Cheng

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.

Find Patent Forward Citations

Quick Actions:

Binek, Lawrence. (2021). Gas turbine engine with a unitary structure and method for manufacturing the same (U.S. Patent No. 11156156). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11156156

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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