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:
Sep. 12, 2023

Filed:

Aug. 20, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Amanda Jean Learned Boucher, Cambridge, MA (US);

Joseph B. Staubach, Colchester, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/115 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02K 3/115 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F05D 2260/232 (2013.01); F05D 2260/606 (2013.01);
Abstract

Aircraft propulsion systems including a closed loop-supercritical fluid system having a turbine, a cooler heat exchanger, a compressor, and a recovery heat exchanger arranged along a closed-loop flow path of a supercritical fluid. A shaft is operably coupled to the turbine and configured to be rotationally driven by the turbine. A fan is configured to generate thrust, the fan operably coupled to the shaft to be rotationally driven by the shaft. A burner is configured to combust a fuel and air from the fan to generate a combusted gas and supply said combusted gas to the recovery heat exchanger of the closed loop-supercritical fluid system and out an exhaust nozzle.


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