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:

Jun. 17, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Honza Stastny, Georgetown, CA;

Robert Sze, Mississauga, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/54 (2006.01); F23R 3/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23R 3/54 (2013.01); F23R 3/002 (2013.01); F23R 3/60 (2013.01); F05D 2240/35 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2260/2214 (2013.01); F05D 2260/22141 (2013.01); F23R 2900/00012 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03044 (2013.01);
Abstract

The described reverse flow combustor of a gas turbine engine includes inner and outer combustor liners defining a combustor chamber therewithin. A large exit duct and a small exit duct are disposed at downstream ends of the outer and inner liner respectively. The small exit duct includes an annular ring removably mounted to a support element of the gas turbine engine and includes a plurality of cooling elements integrally formed with the annular ring and projecting therefrom into impingement airflow. The cooling elements increase the effective surface area of the inner surface of the annular ring, which is adapted to be cooled by the impingement airflow.


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