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. 16, 2019

Filed:

May. 06, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Thomas N. Slavens, Moodus, CT (US);

Mosheshe Camara-Khary Blake, Manchester, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 13/02 (2006.01); F02C 7/18 (2006.01); F02C 3/04 (2006.01); F02C 9/18 (2006.01); F02K 3/115 (2006.01); F02C 6/08 (2006.01); F28F 9/02 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F02C 3/04 (2013.01); F02C 6/08 (2013.01); F02C 7/185 (2013.01); F02C 9/18 (2013.01); F02K 3/115 (2013.01); F28F 9/0278 (2013.01); F05D 2220/32 (2013.01); F05D 2260/20 (2013.01); F05D 2260/213 (2013.01); F28D 2021/0021 (2013.01); F28D 2021/0026 (2013.01); F28F 2270/00 (2013.01); Y02T 50/675 (2013.01);
Abstract

A heat exchanger assembly includes an outer manifold defining an outer cavity. An inner cavity is defined by an inner shell supported within the outer manifold and at least partially surrounded by the outer cavity. The inner shell includes a plurality of impingement openings for directing airflow into the inner cavity. An inner manifold is supported within the inner cavity. The inner manifold is exposed to impingement airflow through the plurality of impingement openings in the inner shell. The inner manifold includes a plurality of flow passages and at least one insulator pocket substantially aligned with the plurality of flow passages. A cooled cooling air system for a gas turbine engine and a gas turbine engine assembly are also disclosed.


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