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. 01, 2026

Filed:

Oct. 11, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventor:

Paul R. Hanrahan, Sedona, AZ (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F02C 6/02 (2006.01); F02C 6/10 (2006.01); H01M 8/0606 (2016.01); H01M 8/12 (2016.01);
U.S. Cl.
CPC ...
F23R 3/28 (2013.01); F02C 6/02 (2013.01); F02C 6/10 (2013.01); H01M 8/0606 (2013.01); H01M 2008/1293 (2013.01); H01M 2250/20 (2013.01);
Abstract

A powerplant for an aircraft includes a first turbine engine, a second turbine engine and a fuel cell system. The second turbine engine includes a second engine flowpath, a second engine compressor section, a second engine combustor section and a second engine turbine section. The second engine flowpath extends from a second engine flowpath inlet to a second engine flowpath outlet. The second engine flowpath inlet and the second engine flowpath outlet are each fluidly coupled with a flowpath of the first turbine engine. The fuel cell system includes a fuel cell, a fuel circuit and an air circuit. The fuel circuit extends through the fuel cell and is fluidly coupled with and upstream of a first fuel injector in the second engine combustor section. The air circuit extends through the fuel cell and is fluidly coupled with and downstream of a bleed from the second engine flowpath.


Find Patent Forward Citations

Hanrahan, Paul. (2026). Aircraft powerplant with boosted turbine engine and fuel cell system (U.S. Patent No. 12723760). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12723760

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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