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. 23, 2024

Filed:

Jul. 08, 2022
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Brian M. Holley, Eastford, CT (US);

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

Marc J. Muldoon, Marlborough, CT (US);

Charles E. Lents, Amston, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/224 (2006.01); F02C 3/20 (2006.01); F02C 7/22 (2006.01); F02C 7/228 (2006.01); F02C 7/232 (2006.01);
U.S. Cl.
CPC ...
F02C 7/224 (2013.01); F02C 3/20 (2013.01); F02C 7/222 (2013.01); F02C 7/228 (2013.01); F02C 7/232 (2013.01);
Abstract

Aircraft propulsion systems and aircraft are described. The aircraft propulsion systems include aircraft systems having at least one hydrogen tank and an aircraft-systems heat exchanger and engine systems having at least a main engine core, a high pressure pump, a hydrogen-air heat exchanger, and an expander, wherein the main engine core comprises a compressor section, a combustor section having a burner, and a turbine section. Hydrogen is supplied from the at least one hydrogen tank through a hydrogen flow path, passing through the aircraft-systems heat exchanger, the high pressure pump, the hydrogen-air heat exchanger, and the expander, prior to being injected into the burner for combustion.


Find Patent Forward Citations

Loading…