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:
Mar. 24, 2026

Filed:

Feb. 07, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Nathan Tomes, Hamilton, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/33 (2024.01); B64D 35/022 (2025.01); B64U 50/11 (2023.01); B64U 50/19 (2023.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F02C 5/00 (2006.01); F02C 6/18 (2006.01);
U.S. Cl.
CPC ...
B64D 27/33 (2024.01); B64D 35/022 (2024.01); B64U 50/11 (2023.01); B64U 50/19 (2023.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F02C 5/00 (2013.01); F02C 6/18 (2013.01); B64D 2221/00 (2013.01);
Abstract

A propulsion system for an aircraft includes an engine assembly and a turbocompressor. The engine assembly includes an engine and an interburner. The engine includes an engine output shaft. The engine is configured to drive rotation of a propulsor with the engine output shaft. The interburner is configured to mix and burn an exhaust gas from the engine with fuel to form a combustion gas. The turbocompressor includes a turbine and a compressor. The turbine and the compressor form a rotational assembly. The rotational assembly includes a shaft, a bladed turbine rotor of the turbine, and a bladed compressor rotor of the compressor. The turbine is connected in fluid communication with the interburner to receive the combustion gas. The compressor is connected in fluid communication with the engine to direct a compressed air to the engine. The rotational assembly is mechanically independent of the engine output shaft.


Find Patent Forward Citations

Tomes, Nathan. (2026). Aircraft propulsion system (U.S. Patent No. 12583596). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12583596

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

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