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:
Sep. 03, 2013

Filed:

Jul. 21, 2010
Applicants:

Thomas J. C. Rogers, San Diego, CA (US);

Christopher Z. Twardochleb, Apline, CA (US);

James W. Blust, San Diego, CA (US);

Mario E. Abreu, Poway, CA (US);

Donald J. Cramb, San Diego, CA (US);

Inventors:

Thomas J. C. Rogers, San Diego, CA (US);

Christopher Z. Twardochleb, Apline, CA (US);

James W. Blust, San Diego, CA (US);

Mario E. Abreu, Poway, CA (US);

Donald J. Cramb, San Diego, CA (US);

Assignee:

Solar Turbines Inc., San Diego, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2006.01); F02C 7/24 (2006.01); F02C 1/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A fuel nozzle for a turbine engine has a central body member with a pilot, a surrounding barrel housing, a mixing duct and an air inlet duct. The fuel nozzle additionally has a main fuel injection device located between the air inlet duct and the mixing duct. The main fuel injection device is configured to introduce a flow of fuel into the barrel member to create a fuel/air mixture which is then premixed with a swirler. The fuel/air mixture then further mixes in the mixing duct and exits the nozzle into a combustor for combustion. The geometry of the fuel nozzle ensures that pressure waves from the combustor do not create a time varying fuel to air equivalence ratio in the flow through the nozzle that achieves a resonance with the pressure waves.


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