U.S. Department of EnergyOffice of Scientific and Technical Information
Self-regulating fuel staging port for turbine combustor
Abstract
A port (60) for axially staging fuel and air into a combustion gas flow path 28 of a turbine combustor (10A). A port enclosure (63) forms an air path through a combustor wall (30). Fuel injectors (64) in the enclosure provide convergent fuel streams (72) that oppose each other, thus converting velocity pressure to static pressure. This forms a flow stagnation zone (74) that acts as a valve on airflow (40, 41) through the port, in which the air outflow (41) is inversely proportion to the fuel flow (25). The fuel flow rate is controlled (65) in proportion to engine load. At high loads, more fuel and less air flow through the port, making more air available to the premixing assemblies (36).
- Inventors:
- Publication Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (USA)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1143661
- Patent Number(s):
- 8,769,955
- Application Number:
- 12/791,975
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Van Nieuwenhuizen, William F., Fox, Timothy A., and Williams, Steven. Self-regulating fuel staging port for turbine combustor. United States: N. p., 2014.
Web.
Van Nieuwenhuizen, William F., Fox, Timothy A., & Williams, Steven. Self-regulating fuel staging port for turbine combustor. United States.
Van Nieuwenhuizen, William F., Fox, Timothy A., and Williams, Steven. 2014.
"Self-regulating fuel staging port for turbine combustor". United States. https://www.osti.gov/servlets/purl/1143661.
@article{osti_1143661,
title = {Self-regulating fuel staging port for turbine combustor},
author = {Van Nieuwenhuizen, William F. and Fox, Timothy A. and Williams, Steven},
abstractNote = {A port (60) for axially staging fuel and air into a combustion gas flow path 28 of a turbine combustor (10A). A port enclosure (63) forms an air path through a combustor wall (30). Fuel injectors (64) in the enclosure provide convergent fuel streams (72) that oppose each other, thus converting velocity pressure to static pressure. This forms a flow stagnation zone (74) that acts as a valve on airflow (40, 41) through the port, in which the air outflow (41) is inversely proportion to the fuel flow (25). The fuel flow rate is controlled (65) in proportion to engine load. At high loads, more fuel and less air flow through the port, making more air available to the premixing assemblies (36).},
doi = {},
url = {https://www.osti.gov/biblio/1143661},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jul 08 00:00:00 EDT 2014},
month = {Tue Jul 08 00:00:00 EDT 2014}
}
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- DiCintio, Richard Martin; Melton, Patrick Benedict
- US Patent Document 9,551,490
Trapped vortex fuel injector and method for manufacture
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- Melton, Patrick Benedict
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