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:
Mar. 03, 2015

Filed:

Jun. 23, 2011
Applicants:

Christopher Zdzislaw Twardochleb, Alpine, CA (US);

Hongyu Wang, San Diego, CA (US);

James Wilfrid Blust, San Diego, CA (US);

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

Inventors:

Christopher Zdzislaw Twardochleb, Alpine, CA (US);

Hongyu Wang, San Diego, CA (US);

James Wilfrid Blust, San Diego, CA (US);

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

Assignee:

Solar Turbines Incorporated, San Diego, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F02G 3/00 (2006.01); F23R 3/14 (2006.01); F23R 3/16 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/14 (2013.01); F23R 3/16 (2013.01); F23R 3/286 (2013.01); F23C 2900/07001 (2013.01); F23D 2900/14021 (2013.01); F23R 2900/00014 (2013.01);
Abstract

A fuel injector for a turbine engine may include a body member disposed about a longitudinal axis, and a barrel member located radially outwardly from the body member. The fuel injector may also include an annular passageway extending between the body member and the barrel member from a first end to a second end. The first end may be configured to be fluidly coupled to a compressor of the turbine engine and the second end may be configured to be fluidly coupled to a combustor of the turbine engine. The fuel injector may also include a perforated plate positioned proximate the first end of the passageway. The perforated plate may be configured to direct compressed air into the annular passageway with a first pressure drop. The fuel injector may also include at least one fuel discharge orifice positioned downstream of the perforated plate. The at least one fuel discharge orifice may be configured to discharge a fuel into the annular passageway with a second pressure drop. The second pressure drop may have a value between about the first pressure drop and about 1.75 times the first pressure drop.


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