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. 02, 2019

Filed:

Jul. 24, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Sri Sreekanth, Mississauga, CA;

Douglas Maccaul, Varennes, CA;

Eduardo Hawie, Woodbridge, CA;

Ion Dinu, Candiac, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/54 (2006.01); F23R 3/60 (2006.01); F23R 3/02 (2006.01); F01D 9/04 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F23R 3/02 (2013.01); F23R 3/54 (2013.01); F05D 2230/232 (2013.01); F05D 2230/80 (2013.01); F05D 2240/35 (2013.01); F23R 3/60 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03041 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine combustor is described which includes outer and inner annular combustor liners formed of sheet metal. The exit duct circumscribes an annular combustor exit and defines a combustion gas path. The exit duct includes a large exit duct having an annular forged metal section which is butt welded at an upstream end to the outer combustor liner to form a first annular joint. The annular forged metal section is fixed at a downstream end to an annular sheet metal wall to form a second annular joint. Methods of forming and of repairing a gas turbine engine combustor are also disclosed.


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