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. 07, 2020

Filed:

Aug. 09, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Gabriel L. Suciu, Glastonbury, CT (US);

Jesse M. Chandler, South Windsor, CT (US);

Federico Papa, Ellington, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 17/14 (2006.01); F01D 25/26 (2006.01); F02C 3/04 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F01D 17/145 (2013.01); F01D 25/26 (2013.01); F02C 3/04 (2013.01); F02C 7/18 (2013.01); F02C 9/18 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/608 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine comprises a core engine housing. A nacelle is positioned radially outwardly of the core engine housing. An outer bypass housing is positioned outwardly of the nacelle. There is at least one accessory to be cooled positioned in a chamber radially between the core engine housing and the nacelle. A manifold delivers cooling air into the chamber, and extends ng circumferentially about a central axis of the core engine. The nacelle has an asymmetric flow cross-section across a circumferential extent.


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