Injection nozzle for a turbomachine
Patent
·
OSTI ID:1078277
A turbomachine includes a compressor, a combustor operatively connected to the compressor, an end cover mounted to the combustor, and an injection nozzle assembly operatively connected to the combustor. The injection nozzle assembly includes a first end portion that extends to a second end portion, and a plurality of tube elements provided at the second end portion. Each of the plurality of tube elements defining a fluid passage includes a body having a first end section that extends to a second end section. The second end section projects beyond the second end portion of the injection nozzle assembly.
- Research Organization:
- General Electric Company (Schenectady, NY)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- FC26-05NT42643
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- 8,261,555
- Application Number:
- 12/832,330
- OSTI ID:
- 1078277
- Country of Publication:
- United States
- Language:
- English
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