Segmented annular combustion system with axial fuel staging
Patent
·
OSTI ID:1651052
A segmented annular combustion system includes an alternating arrangement of fuel nozzles and integrated combustor nozzles. The fuel nozzles deliver fuel to the primary combustion zones. The integrated combustor nozzles include an inner liner segment, an outer liner segment, and a fuel injection panel extending between the liner segments. The fuel injection panel includes injection outlets on one or both side walls to deliver a combustible mixture to the secondary combustion zones. Each fuel injection panel, which provides a boundary between adjacent primary and secondary combustion zones, includes an aft end that defines a turbine nozzle. The segmented annular combustion system is part of a gas turbine.
- Research Organization:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FE0023965
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- 10,690,056
- Application Number:
- 15/464,394
- OSTI ID:
- 1651052
- Country of Publication:
- United States
- Language:
- English
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