Invention Grant
- Patent Title: Closed trapped vortex cavity pilot for a gas turbine engine augmentor
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Application No.: US15085165Application Date: 2016-03-30
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Publication No.: US10704787B2Publication Date: 2020-07-07
- Inventor: David Andrew Perveiler
- 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: General Electric Company
- Agent Pamela Kachur
- Main IPC: F23R3/12
- IPC: F23R3/12 ; F23R3/20 ; F23R3/34 ; F02K3/08 ; F23R3/28 ; F01D9/02 ; F01D25/12 ; F01D25/30 ; F02C7/22 ; F02C7/264 ; F23R3/00 ; F23R3/06 ; F23R3/42

Abstract:
A closed trapped vortex apparatus includes: a tubular structure having a structural wall, the structural wall forming a cavity within the tubular structure, the structural wall having a lower boundary wall forming a boundary between the cavity and a core flow passage; at least one driver hole passing through the structural wall; an ignition source communicating with the cavity; a fuel source communicating with the cavity; and a plurality of flame tubes extending through the lower boundary wall of the tubular structure at preselected locations so as to provide communication between the cavity and the core flow passage.
Public/Granted literature
- US20170284674A1 CLOSED TRAPPED VORTEX CAVITY PILOT FOR A GAS TURBINE ENGINE AUGMENTOR Public/Granted day:2017-10-05
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