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.
Patent No.:
Date of Patent:
Sep. 05, 2017
Filed:
Oct. 03, 2014
Applicant:
Pratt & Whitney Canada Corp., Longueuil, CA;
Inventors:
Yen-Wen Wang, Mississauga, CA;
Nigel Davenport, Hillsburgh, CA;
Assignee:
PRATT & WHITNEY CANADA CORP., Longueuil, CA;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23D 1/00 (2006.01); F23D 11/10 (2006.01); F23D 11/38 (2006.01); F23R 3/28 (2006.01); F23R 3/12 (2006.01);
U.S. Cl.
CPC ...
F23D 11/107 (2013.01); F23D 11/102 (2013.01); F23D 11/103 (2013.01); F23D 11/383 (2013.01); F23R 3/12 (2013.01); F23R 3/286 (2013.01); F23D 2900/14021 (2013.01);
Abstract
A fuel nozzle for a combustor of a gas turbine engine includes a body defining an axial direction and a radial direction, an air passageway defined axially in the body, and a fuel passageway defined axially in the body radially outwardly from the air passageway. The air passageway has a swirl-inducing relief defined at an exit lip of an outer wall of the air passageway. A gas turbine engine and a method of inducing swirl in an air passageway of a fuel nozzle of a gas turbine engine are also presented.