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:
Jan. 30, 2024

Filed:

May. 05, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Hervé Turcotte, Sainte-Julie, CA;

Kenneth Parkman, Halton Hills, CA;

Oleg Morenko, Oakville, CA;

Nicholas Guglielmin, Toronto, CA;

Gavin Kisun, Oakville, CA;

Ryan Miskie, Guelph, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F01D 25/24 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 9/065 (2013.01); F01D 25/162 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); F05D 2240/53 (2013.01); F05D 2260/60 (2013.01);
Abstract

An aircraft engine has: a compressor section having a compressor rotor rotatable about a central axis; a diffuser downstream of the compressor rotor, the diffuser including a diffuser ring extending circumferentially around the central axis; a bearing housing secured to the diffuser ring, the bearing housing contained within a volume located radially inwardly of the diffuser ring; and an air manifold secured to the diffuser ring, the air manifold defining inlets in fluid flow communication with the compressor section and an outlet in fluid flow communication with the volume.


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