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:
Jun. 21, 2016

Filed:

Nov. 26, 2013
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Anthony John Moran, Nuneaton, GB;

Christopher Luke Ford, Dulverton, GB;

Jonathan Frederick Carrotte, Kirby Muxloe, GB;

Alastair Duncan Walker, Loughborough, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23D 14/08 (2006.01); F23D 11/38 (2006.01); F23R 3/28 (2006.01); F23R 3/14 (2006.01); F23R 3/02 (2006.01); F23R 3/34 (2006.01); F23R 3/16 (2006.01);
U.S. Cl.
CPC ...
F23D 11/383 (2013.01); F23R 3/14 (2013.01); F23R 3/286 (2013.01); F05D 2250/14 (2013.01); F05D 2250/141 (2013.01); F23D 2900/11101 (2013.01); F23D 2900/11403 (2013.01); F23R 3/02 (2013.01); F23R 3/16 (2013.01); F23R 3/343 (2013.01);
Abstract

A gas turbine engine lean burn fuel injector includes a fuel injector head which has a first air swirler, a second air swirler arranged around the first air swirler, a pilot fuel injector arranged radially between the first air swirler and the second air swirler. A third air swirler arranged around the second air swirler, a fourth air swirler arranged around the third air swirler and a main fuel injector arranged radially between the third air swirler and the fourth air swirler. A shroud is arranged around the fourth air swirler. A downstream end of the shroud is generally circular in cross-section in a plane perpendicular to the axis (Y) of the fuel injector head and an upstream end of the shroud is generally elliptical in cross-section in a plane perpendicular to the axis (Y) of the fuel injector head.


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