Invention Grant
- Patent Title: Combustor with an igniter provided within at least one of a fuel injector or a compressed air passage
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Application No.: US17589145Application Date: 2022-01-31
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Publication No.: US11795879B2Publication Date: 2023-10-24
- Inventor: Krishnakumar Venkatesan , Michael A. Benjamin , Michael T. Bucaro
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: McGarry Bair PC
- Main IPC: F02C7/266
- IPC: F02C7/266 ; F23R3/28 ; F02C7/232

Abstract:
A turbine engine comprising a compressor section, a combustion section having a combustor, and a turbine section in serial flow arrangement. The combustor having a combustion chamber, at least one fuel injector, at least one compressed air passage, and at least one igniter. The at least one igniter can be provided within a portion of the at least one fuel injector or the at least one compressed air passage.
Public/Granted literature
- US20230193829A1 COMBUSTOR WITH AN IGNITER PROVIDED WITHIN AT LEAST ONE OF A FUEL INJECTOR OR A COMPRESSED AIR PASSAGE Public/Granted day:2023-06-22
Information query
IPC分类: