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:
Dec. 23, 2025

Filed:

May. 15, 2025
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Shailesh Kumar, Bangalore, IN;

Nick Nolcheff, Phoenix, AZ (US);

Tirumala Rao Koka, Phoenix, AZ (US);

Shraman Goswami, Bangalore, IN;

Shakeel Nasir, Phoenix, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/44 (2006.01); F01D 5/04 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); F02C 3/08 (2006.01);
U.S. Cl.
CPC ...
F04D 29/444 (2013.01); F01D 5/048 (2013.01); F01D 5/14 (2013.01); F01D 9/041 (2013.01); F01D 9/045 (2013.01); F02C 3/08 (2013.01); F04D 29/441 (2013.01);
Abstract

Diffusers are provided for gas turbine engines downstream of an impeller of a centrifugal compressor. The diffusers include a diffuser flowbody having an inner and outer peripheral portions, diffuser passages extending through the diffuser flowbody that include passage inlets and outlets formed in the inner and outer peripheral portions, respectively, and diffuser vanes contained in the diffuser flowbody and partitioning the diffuser passages. Each of the diffuser vanes include a first vane sidewall, a second vane sidewall opposite the first vane sidewall, a hub-side endwall, and a shroud-side endwall opposite the hub-side endwall. Each of the diffuser vanes have a thickness between the first sidewall and the second sidewall and a tapered cross-sectional profile portion that decreases from the shroud-side endwall to the hub-side endwall.


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