Invention Grant
- Patent Title: Torch igniter cooling system
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Application No.: US17089250Application Date: 2020-11-04
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Publication No.: US11415057B2Publication Date: 2022-08-16
- Inventor: Jason Ryon , Lev Alexander Prociw
- Applicant: Delavan Inc.
- Applicant Address: US IA Des Moines
- Assignee: Delavan Inc.
- Current Assignee: Delavan Inc.
- Current Assignee Address: US IA Des Moines
- Agency: Kinney & Lange, P.A.
- Main IPC: F02C7/00
- IPC: F02C7/00 ; F02C7/264 ; F23R3/06 ; F23D14/78 ; B33Y80/00

Abstract:
An embodiment of a torch igniter for a combustor of a gas turbine engine includes a combustion chamber oriented about an axis, a cap defining the axially upstream end of the combustion chamber and situated on the axis, a tip defining the axially downstream end of the combustion chamber, an igniter wall extending from the cap to the tip and defining a radial extent 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, wherein the outlet passage fluidly connects the combustion chamber to the combustor of the gas turbine engine, and a cooling system. The cooling system has an air inlet, a cooling channel, and an aperture. The cooling channel forms a flow path having a first axial section, a second axial section, a radially inward section, and a radially outward section.
Public/Granted literature
- US11473505B2 Torch igniter cooling system Public/Granted day:2022-10-18
Information query
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