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:
Apr. 02, 2019

Filed:

May. 08, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventor:

Christopher B. Lyons, West Hartford, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 25/08 (2006.01); F02C 7/12 (2006.01); F01D 25/16 (2006.01); F01D 9/06 (2006.01); F01D 5/02 (2006.01); F01D 9/02 (2006.01); F01D 25/12 (2006.01); F01D 25/24 (2006.01); F02C 3/06 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 5/02 (2013.01); F01D 9/02 (2013.01); F01D 9/065 (2013.01); F01D 25/08 (2013.01); F01D 25/12 (2013.01); F01D 25/162 (2013.01); F01D 25/24 (2013.01); F02C 3/06 (2013.01); F02C 7/04 (2013.01); F02C 7/12 (2013.01); F02C 7/185 (2013.01); F05D 2210/12 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3219 (2013.01); F05D 2240/12 (2013.01); F05D 2240/35 (2013.01); F05D 2260/211 (2013.01); F05D 2260/213 (2013.01); Y02T 50/676 (2013.01);
Abstract

An inner diffuser case for a turbine engine includes a fore gas path edge and an aft gas path edge defining a strut, wherein each of the fore gas path edge and the aft gas path edge include a gas path opening, a support cone structure extending radially outward from the strut, wherein the support cone structure is operable to structurally connect the strut to a turbine engine case, a diffuser case skirt structure extending radially inward from the strut, wherein the diffuser case skirt structure is operable to structurally connect the diffuser case strut to an inner support structure of the turbine engine, and at least one direct feed air passage passing radially through the strut including a radially outward upper mixing chamber opening and a radially inward direct air feed opening, the direct air feed opening is connected to a direct air feed.


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