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.
Patent No.:
Date of Patent:
Jun. 17, 2025
Filed:
Apr. 25, 2024
Gulfstream Aerospace Corporation, Savannah, GA (US);
Derek Muzychka, Savannah, GA (US);
Donald Freund, Savannah, GA (US);
Andrew Clemens, Savannah, GA (US);
John Louis, Savannah, GA (US);
Joseph Gavin, Savannah, GA (US);
Till Gerhardt, Savannah, GA (US);
William Mcfarland, Savannah, GA (US);
Benjamin Walke, Savannah, GA (US);
GULFSTREAM AEROSPACE CORPORATION, Savannah, GA (US);
Abstract
Various non-limiting embodiments of a nozzle assembly for use with a propulsion system and a sleeve assembly for use with the nozzle assembly are disclosed herein. In a non-limiting embodiment, the nozzle assembly includes, but is not limited to, a nacelle. The nozzle assembly further includes, but is not limited to, a sleeve assembly mounted within the nacelle downstream of the engine. The sleeve assembly is configured to receive the mass flow from the engine and to guide the mass flow to an exit of the propulsion system. The sleeve assembly is comprised of a plurality of sleeve segments arranged in a circumferential configuration. Each sleeve segment of the plurality of sleeve segments has an elongate body that is longitudinally aligned with a longitudinal axis of the sleeve assembly.