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:
Nov. 08, 2022

Filed:

Mar. 26, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Paul W. Duesler, Manchester, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F28F 7/00 (2006.01); F02C 7/18 (2006.01); F02K 3/115 (2006.01); F02C 7/141 (2006.01); F02C 7/20 (2006.01); F04D 29/58 (2006.01); F28D 1/047 (2006.01); F28D 7/06 (2006.01); F28F 21/08 (2006.01); F28F 9/013 (2006.01); F28D 21/00 (2006.01); F04D 19/02 (2006.01); F28F 9/22 (2006.01);
U.S. Cl.
CPC ...
F02C 7/185 (2013.01); F02C 7/141 (2013.01); F02C 7/18 (2013.01); F02C 7/20 (2013.01); F02K 3/115 (2013.01); F04D 29/5826 (2013.01); F28D 1/0475 (2013.01); F28D 7/06 (2013.01); F28F 9/0131 (2013.01); F28F 21/081 (2013.01); F04D 19/02 (2013.01); F05D 2260/213 (2013.01); F28D 2021/0026 (2013.01); F28F 2009/222 (2013.01); F28F 2009/226 (2013.01); F28F 2245/00 (2013.01); F28F 2250/06 (2013.01); F28F 2255/00 (2013.01); F28F 2265/26 (2013.01); F28F 2280/00 (2013.01);
Abstract

A heat exchanger (HEX) for cooling air in a gas turbine engine is provided. The HEX may comprise a central manifold comprising an inlet portion, a first outlet portion, and a second outlet portion. The HEX may further comprise a plurality of tubes coupled to the central manifold, the plurality of tubes comprising at least a first tube, a second tube, a third tube, and a fourth tube, a shroud at least partially encasing said plurality of tubes, and a cooling air flow path defined by at least one of the shroud, the plurality of tubes, and an outer surface of the central manifold, wherein the cooling air flow path is orthogonal to said plurality of tubes.


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