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:
May. 14, 2024

Filed:

Nov. 09, 2022
Applicant:

Collins Engine Nozzles, Inc., Des Moines, IA (US);

Inventors:

Jason Ryon, Carlisle, IA (US);

Lev Alexander Prociw, Johnston, IA (US);

Assignee:

Collins Engine Nozzles, Inc., Des Moines, IA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/264 (2006.01); F02C 7/18 (2006.01); F23R 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/264 (2013.01); F02C 7/18 (2013.01); F23R 3/06 (2013.01); F23R 2900/00009 (2013.01); F23R 2900/03043 (2013.01);
Abstract

An embodiment of a torch igniter for a combustor of a gas turbine engine comprises a combustion chamber oriented about an axis, a cap defining an axially upstream end of the combustion chamber and oriented about the axis, a tip defining an axially downstream end of the combustion chamber, a structural wall coaxial with and surrounding the igniter wall, an outlet passage defined by the igniter wall within the tip, and a cooling system. The cooling system comprises an air inlet formed within the structural wall, a first flow path disposed between the structural wall and the igniter wall, and an aperture extending through the igniter wall transverse to the flow direction. The aperture directly fluidly connects the first flow path to the combustion chamber.


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