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:
Jul. 23, 2019

Filed:

Jan. 26, 2016
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Raymond Gage, Phoenix, AZ (US);

Bruce David Reynolds, Chandler, AZ (US);

Jeffrey D. Harrison, Mesa, AZ (US);

Michael Todd Barton, Phoenix, AZ (US);

Mahmoud Mansour, Phoenix, AZ (US);

Kent L. Kime, Phoenix, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 13/02 (2006.01); F04D 29/42 (2006.01); F04D 29/28 (2006.01); F04D 29/58 (2006.01); F02C 3/08 (2006.01); F02C 6/08 (2006.01); F04D 29/44 (2006.01);
U.S. Cl.
CPC ...
F04D 29/4206 (2013.01); F02C 3/08 (2013.01); F02C 6/08 (2013.01); F04D 29/284 (2013.01); F04D 29/444 (2013.01); F04D 29/582 (2013.01); F05D 2220/32 (2013.01); F05D 2240/128 (2013.01); F05D 2240/30 (2013.01); F05D 2260/20 (2013.01);
Abstract

Embodiments of an impeller shroud support for disposition around an impeller are provided, as are embodiments of gas turbine engine including impeller shroud supports. In one embodiment, the impeller shroud support includes a shroud body, a support arm joined to and extending around the shroud body, and a plurality of Mid-Impeller Bleed (MIB) flow passages. Each MIB flow passage includes, in turn, an inlet formed in the shroud body and configured to receive bleed air extracted from the impeller, a throat portion, an outlet formed in the support arm and through which the bleed air is discharged, and a curved intermediate section between the inlet and the outlet. During usage of the impeller shroud support, the curved intermediate section turns the bleed air flowing through the MIB passage in a radially outward direction prior to discharge from the outlet of the MIB flow passage.


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