Injector with integrated resonator
Abstract
The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.
- Inventors:
- Issue Date:
- Research Org.:
- National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1149997
- Patent Number(s):
- 8789372
- Application Number:
- 12/499,777
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Johnson, Thomas Edward, Ziminsky, Willy Steve, York, William David, and Stevenson, Christian Xavier. Injector with integrated resonator. United States: N. p., 2014.
Web.
Johnson, Thomas Edward, Ziminsky, Willy Steve, York, William David, & Stevenson, Christian Xavier. Injector with integrated resonator. United States.
Johnson, Thomas Edward, Ziminsky, Willy Steve, York, William David, and Stevenson, Christian Xavier. Tue .
"Injector with integrated resonator". United States. https://www.osti.gov/servlets/purl/1149997.
@article{osti_1149997,
title = {Injector with integrated resonator},
author = {Johnson, Thomas Edward and Ziminsky, Willy Steve and York, William David and Stevenson, Christian Xavier},
abstractNote = {The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {7}
}
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