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. 19, 2023

Filed:

Sep. 02, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Jose R. Paulino, Jupiter, FL (US);

Lawrence A. Binek, Glastonbury, CT (US);

Sean R. Jackson, Palm City, FL (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/02 (2006.01); F02C 3/08 (2006.01);
U.S. Cl.
CPC ...
F02K 3/02 (2013.01); F02C 3/085 (2013.01); F05D 2240/128 (2013.01); F05D 2240/35 (2013.01); F05D 2260/606 (2013.01);
Abstract

A gas turbine engine is provided that includes an engine core and a bypass duct. The engine core includes a compressor section, a combustor section, a turbine section and a core flowpath. The compressor section includes a radial flow compressor rotor. The core flowpath extends through the compressor section, the combustor section and the turbine section from a core inlet to a core exhaust. The bypass duct includes a bypass flowpath that extends outside of the engine core from a bypass inlet to a bypass exhaust. The bypass inlet is disposed along the compressor section and fluidly coupled with core flowpath.


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