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. 25, 2026

Filed:

Aug. 28, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jocelyn Bisson, Saint-Basile-le-Grand, CA;

Guy Lefebvre, St-Bruno, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 5/02 (2006.01);
U.S. Cl.
CPC ...
F01D 11/001 (2013.01); F01D 5/02 (2013.01); F05D 2240/55 (2013.01); F05D 2250/711 (2013.01); F05D 2250/712 (2013.01);
Abstract

An assembly is provided for an aircraft powerplant. This powerplant assembly includes a bladed rotor and a stationary structure. The bladed rotor is rotatable about an axis. The bladed rotor includes a rotor disk and a plurality of rotor blades. The rotor disk includes a web and a rim with a concave disk surface at an inside corner between the web and the rim. The concave disk surface has a disk surface sectional geometry in a reference plane parallel with the axis. The rotor blades are arranged circumferentially around and project radially out from the rim. The stationary structure includes a lip with a convex lip surface. The convex lip surface is next to the concave disk surface. The convex lip surface has a lip surface sectional geometry in the reference plane that matches the disk surface sectional geometry.


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