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Title: 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 Co., 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
Resource Relation:
Patent File Date: 03/21/2017
Country of Publication:
United States
Language:
English

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