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:
Dec. 29, 2015

Filed:

Dec. 23, 2011
Applicant:

Timothy C. Roesler, Plainfield, IN (US);

Inventor:

Timothy C. Roesler, Plainfield, IN (US);

Assignee:

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/30 (2006.01); F02C 9/28 (2006.01); F02C 9/48 (2006.01); F23K 5/14 (2006.01); F23N 1/00 (2006.01);
U.S. Cl.
CPC ...
F23R 3/30 (2013.01); F02C 9/28 (2013.01); F02C 9/48 (2013.01); F23K 5/14 (2013.01); F23N 1/002 (2013.01); F23K 2301/10 (2013.01); F23K 2301/20 (2013.01); F23N 2041/20 (2013.01);
Abstract

An apparatus is disclosed including a main fuel supply fluidly coupled to a main fuel valve and an arcuate fuel passage receiving main fuel through the main fuel valve. The arcuate fuel passage includes a passage diameter and a radius of curvature which provides sufficient rotational acceleration to the main fuel such that a liquid portion of the main fuel is deposited on an outer wall of the arcuate fuel passage. The apparatus includes a fuel injector nozzle that receives the main fuel from the arcuate fuel passage, and injects the main fuel into a combustion chamber for a turbine engine. The apparatus further includes a pilot fuel supply fluidly coupled to a pilot fuel passage and a fuel selector structured to selectively provide the main fuel or the pilot fuel to the fuel injector nozzle.


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