Integrated combustor nozzle for a segmented annular combustion system
Patent
·
OSTI ID:1637763
The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbine nozzle.
- Research Organization:
- General Electric Company, Schenectady, NY (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FE0023965
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- 10,605,459
- Application Number:
- 15/464,419
- OSTI ID:
- 1637763
- Country of Publication:
- United States
- Language:
- English
Similar Records
Cooling of integrated combustor nozzle of segmented annular combustion system
Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
Mounting of integrated combustor nozzles in a segmented annular combustion system
Patent
·
Tue May 05 00:00:00 EDT 2020
·
OSTI ID:1650855
Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
Patent
·
Tue Mar 10 00:00:00 EDT 2020
·
OSTI ID:1637865
Mounting of integrated combustor nozzles in a segmented annular combustion system
Patent
·
Tue Mar 10 00:00:00 EDT 2020
·
OSTI ID:1637866