Invention Grant
- Patent Title: Combustor for a gas turbine
-
Application No.: US16068708Application Date: 2017-01-13
-
Publication No.: US10859272B2Publication Date: 2020-12-08
- Inventor: Suresh Sadasivuni
- Applicant: Siemens Aktiengesellschaft
- Applicant Address: DE Munich
- Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee Address: DE Munich
- Priority: EP16151603 20160115
- International Application: PCT/EP2017/050705 WO 20170113
- International Announcement: WO2017/121872 WO 20170720
- Main IPC: F23R3/34
- IPC: F23R3/34 ; F23R3/14 ; F23R3/28 ; F23C7/00 ; F23D11/38

Abstract:
A combustor for a gas turbine, having a pre-combustion chamber having a peripheral wall around a center axis of the pre-combustion chamber, the peripheral wall has an inner panel and an outer panel and a passage provided between the inner and the outer panels, a swirler which is connected to the pre-combustion chamber for providing pre-combustion chamber with a flow of an oxidant gas, at least a pilot fuel injector, wherein the swirler is connected to the peripheral wall in such a way that a portion of the oxidant gas from the swirler is channeled to the passage, and the pilot fuel injector is connected to the passage for injecting a flow of pilot fuel into the passage.
Public/Granted literature
- US20190024901A1 COMBUSTOR FOR A GAS TURBINE Public/Granted day:2019-01-24
Information query