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:
Mar. 31, 2026

Filed:

Feb. 21, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Hien Duong, Mississauga, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/28 (2006.01); B64C 11/00 (2006.01); F01D 5/04 (2006.01); F02C 3/08 (2006.01); F02C 3/14 (2006.01); F04D 1/00 (2006.01); F04D 29/44 (2006.01);
U.S. Cl.
CPC ...
F04D 29/284 (2013.01); B64C 11/001 (2013.01); F01D 5/04 (2013.01); F04D 1/00 (2013.01); F04D 29/441 (2013.01);
Abstract

An impeller is provided for a centrifugal compressor of an aircraft engine. The impeller includes an impeller hub and an impeller shroud having an inducer portion, an exducer portion and a bend portion interposed between the inducer portion and the exducer portion. The impeller shroud is swept forwardly in the exducer portion, the impeller shroud and the impeller hub define a gap extending through the inducer portion, the bend portion and the exducer portion and the gap is characterized as having a passage area that exhibits about a 34.375% increase from 10% of the shroud chord to 45% of the shroud chord and exhibits about a −31.1628% decrease from 45% of the shroud chord to 92.5% of the shroud chord.


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