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:
Jul. 10, 2018

Filed:

Apr. 25, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Remo Marini, Lasalle, CA;

Mark Huzzard Cunningham, Montreal, CA;

Francois C. Bisson, Vallee-Jonction, CA;

Reza Mohammad Kameshki, Toronto, CA;

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/38 (2006.01); F02K 1/48 (2006.01); F02K 3/06 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F02K 1/48 (2013.01); F01D 9/041 (2013.01); F02K 1/386 (2013.01); F02K 3/06 (2013.01); F05D 2210/40 (2013.01); F05D 2250/61 (2013.01);
Abstract

A turbine exhaust case (TEC) of a turbofan aeroengine includes a mixer for mixing exhaust gases with a bypass air stream, the TEC comprising an annular hub and the mixer surrounding the hub, and a plurality of deswirling struts circumferentially spaced apart with respect to a central axis of the TEC and located entirely within an axial length of the mixer. The mixer defines a trailing edge having one or more upstream-most locations thereof where the mixing of the exhausted gases and the bypass air stream begins to take place. The deswirling struts each extend radially across the annular exhaust gas duct and interconnect the mixer and the hub, defining a trailing edge positioned upstream of and axially spaced away from the one or more upstream-most locations of the trailing edge of the mixer.


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