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:
Aug. 12, 2025

Filed:

Jun. 26, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

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

Daniel B. Kupratis, Wallingford, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/20 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 29/00 (2006.01); B64D 35/00 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 29/00 (2013.01); B64D 35/00 (2013.01); F02C 6/206 (2013.01); B64D 27/026 (2024.01); B64D 2221/00 (2013.01); F05D 2220/323 (2013.01); F05D 2220/74 (2013.01); F05D 2220/76 (2013.01);
Abstract

An aircraft system is provided that includes a first gas turbine engine, a propulsor rotor, a second gas turbine engine, an electric generator and an electric component. The first gas turbine engine includes a first compressor section, a first combustor section, a first turbine section and a first flowpath. The propulsor rotor is rotatably driven by the first gas turbine engine. The second gas turbine engine includes a second compressor section, a second combustor section, a second turbine section and a second flowpath between a second inlet and a second exhaust. The second inlet and the second exhaust are each fluidly coupled with the first flowpath upstream of a combustor of the first combustor section. The electric generator is rotatably driven by the second gas turbine engine. The electric component receives electricity generated by the electric generator. The electric component is discrete from the first gas turbine engine.


Find Patent Forward Citations

Loading…