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:
Jul. 09, 2024

Filed:

Sep. 23, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Stephen H. Taylor, East Hartford, CT (US);

Alan Retersdorf, Avon, CT (US);

Oliver V. Atassi, Longmeadow, MA (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02C 3/10 (2006.01); F02C 7/18 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F02C 6/08 (2013.01); F02C 3/10 (2013.01); F02C 7/18 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/18 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01);
Abstract

An aircraft propulsion system includes a core engine that includes a core flow path where a core airflow is compressed in a compressor section, communicated to a combustor section, mixed with fuel and ignited to generate a gas flow that is expanded through a turbine section for powering a primary propulsor. The aircraft propulsion system further includes a tap that is at a location upstream of the combustor section where a bleed airflow is drawn, a heat exchanger where the bleed airflow is heated by the gas flow, a power turbine through which heated bleed airflow is expanded to generate a work output, and a secondary propulsor that is driven by the work output that is generated by the power turbine.


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