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:
Oct. 20, 2026

Filed:

Jun. 14, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Remo Marini, Lasalle, CA;

Sami Girgis, L'orignal, CA;

Amin Afroosheh, Candiac, CA;

Guy Lefebvre, St-Bruno, CA;

Remy Synnott, St-Jean-sur-Richelieu, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 5/22 (2006.01); F01D 11/00 (2006.01); F01D 11/02 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 5/225 (2013.01); F01D 11/001 (2013.01); F01D 11/02 (2013.01); F01D 25/24 (2013.01);
Abstract

A shrouded turbine assembly for a gas turbine engine is provided that includes a rotor assembly and a forward vane assembly. The rotor assembly has a plurality of rotor blades circumferentially distributed around a disk. Each rotor blade extends from the disk to a shrouded end, and each rotor blade has a shroud disposed at the shrouded end. The forward vane assembly is disposed forward of the rotor assembly. The forward vane assembly has a plurality of first vanes disposed in an annular configuration, with each first vane extending between a first vane inner radial platform to a first vane outer radial platform. The forward vane assembly includes an outer radial casing that includes a casing segment and an air diverter. The air diverter extends axially and is disposed radially outside of the shroud of each rotor blade of the plurality of rotor blades.


Find Patent Forward Citations

Marini, Remo. (2026). Shrouded turbine assembly for gas turbine engine (U.S. Patent No. 12768282). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12768282

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

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