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:
Feb. 04, 2025

Filed:

Aug. 29, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Neil J. Terwilliger, Cheshire, CT (US);

Lance L. Smith, West Hartford, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/141 (2006.01); F02C 3/06 (2006.01); F02C 7/143 (2006.01); F02C 7/16 (2006.01);
U.S. Cl.
CPC ...
F02C 7/1435 (2013.01); F02C 3/06 (2013.01); F02C 7/16 (2013.01); F05D 2220/323 (2013.01); F05D 2260/212 (2013.01); F05D 2260/609 (2013.01);
Abstract

An aircraft propulsion system includes a compressor section where an inlet airflow is compressed, a combustor section where the compressed inlet airflow is mixed with fuel and ignited to generate an exhaust gas flow that is communicated through a core flow path, a turbine section through which the exhaust gas flow expands to generate a mechanical power output, the exhaust gas flow is split into at least a first exhaust gas flow and a second exhaust gas flow, and a condenser where water is extracted from the second exhaust gas flow, and a first heat exchanger where at least a portion of the extracted water is utilized for cooling a core flow along the core flow path.


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