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:
Oct. 01, 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 ...
B64D 37/30 (2006.01); B64D 37/34 (2006.01); B64D 41/00 (2006.01); F02C 3/22 (2006.01); F02C 7/224 (2006.01); F02C 7/32 (2006.01);
U.S. Cl.
CPC ...
B64D 37/30 (2013.01); B64D 37/34 (2013.01); B64D 41/00 (2013.01); F02C 3/22 (2013.01); F02C 7/224 (2013.01); F02C 7/32 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/40311 (2013.01);
Abstract

Aircraft propulsion systems have aircraft systems including at least one hydrogen tank and an aircraft-systems heat exchanger and engine systems includes at least a main engine core, a high pressure pump, a hydrogen-air heat exchanger, and a turbo expander. The main engine core includes a compressor section, a combustor section having a burner, and a turbine section arranged along an engine shaft. 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 turbo expander, prior to being injected into the burner for combustion. The turbo expander is configured to impart power to the engine shaft.


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