Injection nozzle for a turbomachine
Abstract
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.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1078277
- Patent Number(s):
- 8261555
- Application Number:
- 12/832,330
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23D - BURNERS
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23G - CREMATION FURNACES
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Uhm, Jong Ho, Johnson, Thomas Edward, and Kim, Kwanwoo. Injection nozzle for a turbomachine. United States: N. p., 2012.
Web.
Uhm, Jong Ho, Johnson, Thomas Edward, & Kim, Kwanwoo. Injection nozzle for a turbomachine. United States.
Uhm, Jong Ho, Johnson, Thomas Edward, and Kim, Kwanwoo. Tue .
"Injection nozzle for a turbomachine". United States. https://www.osti.gov/servlets/purl/1078277.
@article{osti_1078277,
title = {Injection nozzle for a turbomachine},
author = {Uhm, Jong Ho and Johnson, Thomas Edward and Kim, Kwanwoo},
abstractNote = {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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2012},
month = {9}
}
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