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:
Aug. 13, 2019

Filed:

Oct. 25, 2013
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Tin Cheung John Hu, Markham, CA;

Oleg Morenko, Oakville, CA;

Lev Alexander Prociw, Johnston, IA (US);

Parham Zabeti, Toronto, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/50 (2006.01); F23R 3/00 (2006.01); F23R 3/28 (2006.01); F23R 3/08 (2006.01);
U.S. Cl.
CPC ...
F23R 3/06 (2013.01); F23R 3/28 (2013.01); F23R 3/283 (2013.01); F23R 3/286 (2013.01); F23R 3/50 (2013.01); F23R 3/002 (2013.01); F23R 3/08 (2013.01);
Abstract

In a gas turbine combustor having an inner and outer liner defining an annular combustion chamber, at least an annular scoop ring provided on each inner and outer combustor liner. The annular scoop ring includes a solid radial inner base provided with bores defined therein and communicating with the combustion chamber to form air dilution inlets. The scoop ring has a radial outer portion in the form of a C-shaped scoop open to receive high velocity annular air flow. The bores of the inlets communicating with the scoop portion to direct the air flow into the combustion chamber whereby the bores of the inlets form jet nozzles to generate air jet penetration and direction within the combustion chamber.


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