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:
Sep. 19, 2017

Filed:

Feb. 28, 2011
Applicants:

Andreas Eleftheriou, Woodbridge, CA;

David Menheere, Georgetown, CA;

Daniel Alecu, Toronto, CA;

Darius Jehangir Karanjia, Mississauga, CA;

Daniel Van Den Ende, Mississauga, CA;

Inventors:

Andreas Eleftheriou, Woodbridge, CA;

David Menheere, Georgetown, CA;

Daniel Alecu, Toronto, CA;

Darius Jehangir Karanjia, Mississauga, CA;

Daniel Van Den Ende, Mississauga, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, Quebec, unknown;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/08 (2006.01); F28D 21/00 (2006.01); F02C 7/10 (2006.01); F02C 7/143 (2006.01); F28D 9/00 (2006.01);
U.S. Cl.
CPC ...
F28D 21/0003 (2013.01); F02C 7/08 (2013.01); F02C 7/10 (2013.01); F02C 7/143 (2013.01); F28D 9/0018 (2013.01); F28F 2265/26 (2013.01); F28F 2265/30 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine recuperator recuperator including exhaust passages providing fluid flow communication between an exhaust inlet and an exhaust outlet, the exhaust inlet being oriented to receive exhaust flow from a turbine of the engine and the exhaust outlet being oriented to deliver the exhaust flow to atmosphere, the exhaust passages having an arcuate profile in a plane perpendicular to a central axis of the recuperator to reduce a swirl of the exhaust flow. Air passages are in heat exchange relationship with the exhaust passages and providing fluid flow communication between an air inlet and an air outlet, design to sealingly respective plenum of the gas turbine engine.


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