Invention Grant
- Patent Title: Combustor having dilution cooled liner
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Application No.: US17932806Application Date: 2022-09-16
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Publication No.: US12055293B2Publication Date: 2024-08-06
- Inventor: Perumallu Vukanti , Karthikeyan Sampath , Pradeep Naik , Ranganatha Narasimha Chiranthan , Rimple Rangrej , Hiranya Nath , Ravindra Shankar Ganiger
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US OH Cincinnati
- Agency: Venable LLP
- Agent Griffin A. A. Deadwick; Michele V. Frank
- Priority: IN 2211029740 2022.05.24
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00

Abstract:
A combustor for a gas turbine has a combustor liner including an upstream liner portion, and a downstream liner portion. The upstream liner portion includes an outer shell and a heat shield panel, with a baffle cavity therebetween. The outer shell includes an outer shell cooling opening for providing a flow of compressed air to the baffle cavity, and the heat shield panel includes a heat shield panel cooling opening at a downstream end of the heat shield panel. A fence is arranged at a downstream side of the heat shield panel cooling opening and extends beyond a hot side surface of the heat shield panel into a combustion chamber. The heat shield panel cooling opening provides a flow of the compressed air therethrough from the baffle cavity for cooling of the heat shield panel and for providing at least partial dilution of combustion gases within the combustion chamber.
Public/Granted literature
- US20230383949A1 COMBUSTOR HAVING DILUTION COOLED LINER Public/Granted day:2023-11-30
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