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:
Feb. 18, 2025

Filed:

Aug. 14, 2023
Applicant:

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Kenneth M. Pesyna, Indianapolis, IN (US);

Andrew M. Simonich, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/60 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/60 (2013.01); F02K 1/763 (2013.01);
Abstract

A propulsion unit includes a gas turbine engine and an exhaust nozzle coupled to an aft end of the gas turbine engine. The exhaust nozzle is configured to interact with exhaust gases exiting the gas turbine engine in an aft direction. The exhaust nozzle includes an outer nozzle case and an inner plug that cooperate to define an exhaust flow path therebetween. The exhaust nozzle is configured to manipulate the exhaust gases to provide different thrust capabilities for the gas turbine engine.


Find Patent Forward Citations

Pesyna, Kenneth. (2025). Plug nozzle and thrust reverser for high mach gas turbine engines (U.S. Patent No. 12228096). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12228096

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

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