scholarly journals A Detailed Characterization of the Velocity and Thermal Fields in a Model Can Combustor With Wall Jet Injection

1989 ◽  
Vol 111 (1) ◽  
pp. 31-35 ◽  
Author(s):  
C. D. Cameron ◽  
J. Brouwer ◽  
C. P. Wood ◽  
G. S. Samuelsen
Keyword(s):  
Gas Turbine ◽  
Liquid Fuel ◽  
Fuel Injection ◽  
Wall Jet ◽  
Gas Turbine Combustor ◽  
Jet Interaction ◽  
Thermal Fields ◽  
Air Mixing ◽  
Model Gas Turbine Combustor

This work represents a first step in the establishment of a data base to study the interaction and influence of liquid fuel injection, wall jet interaction, and dome geometry on the fuel air mixing process in a flowfield representative of a practical combustor. In particular, the aerodynamic and thermal fields of a model gas turbine combustor are characterized via detailed spatial maps of velocity and temperature. Measurements are performed at an overall equivalence ratio of 0.3 with a petroleum JP-4 fuel. The results reveal that the flowfield characteristics are significantly altered in the presence of reaction. Strong on-axis backmixing in the dome region, present in the isothermal flow, is dissipated in the case of reaction. The thermal field exhibits the primary, secondary, and dilution zone progression of temperatures characteristic of practical gas turbine combustors. A parametric variation on atomizing air reveals a substantial sensitivity of the mixing in this flow to nozzle performance and spray symmetry.

scholarly journals Response of a Model Gas Turbine Combustor to Variation in Gaseous Fuel Composition

2000 ◽  
Vol 123 (4) ◽  
pp. 824-831 ◽  
Author(s):  
R. M. Flores ◽  
M. M. Miyasato ◽  
V. G. McDonell ◽  
G. S. Samuelsen
Keyword(s):  
Gas Turbine ◽  
Fuel Injection ◽  
Injection System ◽  
Fuel Composition ◽  
Gas Turbine Combustor ◽  
Fuel Distribution ◽  
Air Mixing ◽  
Predominant Factor ◽  
Model Gas Turbine Combustor ◽  
Composition Changes

The effect of fuel composition on performance is evaluated on a model gas turbine combustor designed to mimic key features of practical devices. A flexible fuel injection system is utilized to control the placement of the fuel in the device to allow exploration and evaluation of fuel distribution effects in addition to chemistry effects. Gas blends reflecting the extremes in compositions found in the U.S. are considered. The results illustrate that, for the conditions and configuration studied, both fuel chemistry and fuel air mixing play a role in the performance of the device. While chemistry appears to be the predominant factor in stability, a role is noted in emissions performance as well. It is also found that changes in fuel distribution associated with changes in fuel momentum for fixed firing rate also have an impact on emissions. For the system considered, a strategy for sustaining optimal performance while fuel composition changes is illustrated.

scholarly journals Response of a Model Gas Turbine Combustor to Variation in Gaseous Fuel Composition

2000 ◽  
Author(s):  
R. M. Flores ◽  
M. M. Miyasato ◽  
V. G. McDonell ◽  
G. S. Samuelsen
Keyword(s):  
Gas Turbine ◽  
Fuel Injection ◽  
Injection System ◽  
Fuel Composition ◽  
Gas Turbine Combustor ◽  
Fuel Distribution ◽  
Air Mixing ◽  
Predominant Factor ◽  
Model Gas Turbine Combustor ◽  
Composition Changes

The effect of fuel composition on performance is evaluated on a model gas turbine combustor designed to mimic key features of practical devices. A flexible fuel injection system is utilized to control the placement of the fuel in the device to allow exploration and evaluation of fuel distribution effects in addition to chemistry effects. Gas blends reflecting the extremes in compositions found in the U.S. are considered. The results illustrate that, for the conditions and configuration studied, both fuel chemistry and fuel air mixing play a role in the performance of the device. While chemistry appears to be the predominant factor in stability, a role is noted in emissions performance as well. It is also found that changes in fuel distribution associated with changes in fuel momentum for fixed firing rate also have an impact on emissions. For the system considered, a strategy for sustaining optimal performance while fuel composition changes is illustrated.

scholarly journals Impact of Ethane and Propane Variation in Natural Gas on the Performance of a Model Gas Turbine Combustor

2003 ◽  
Vol 125 (3) ◽  
pp. 701-708 ◽  
Author(s):  
R. M. Flores ◽  
V. G. McDonell ◽  
G. S. Samuelsen
Keyword(s):  
Natural Gas ◽  
Gas Turbine ◽  
Statistical Approach ◽  
Present System ◽  
Fuel Composition ◽  
Gas Turbine Combustor ◽  
Air Mixing ◽  
Gas Fuel ◽  
Model Gas Turbine Combustor ◽  
The Impact

In the area of stationary power generation, there exists a growing interest in understanding the role that gaseous fuel composition plays on the performance of natural gas-fired gas turbine systems. In this study, an atmospherically fired model gas turbine combustor with a fuel flexible fuel/air premixer is employed to investigate the impact of significant amounts of ethane and propane addition into a baseline natural gas fuel supply. The impacts of these various fuel compositions, in terms of the emissions of NOx and CO, and the coupled impact of the degree of fuel/air mixing, are captured explicitly for the present system by means of a statistically oriented testing methodology. These explicit expressions are also compared to emissions maps that encompass and expand beyond the statistically based test matrix to verify the validity of the employed statistical approach.

scholarly journals Impact of Ethane and Propane Variation in Natural Gas on the Performance of a Model Gas Turbine Combustor

2002 ◽  
Author(s):  
R. M. Flores ◽  
V. G. McDonell ◽  
G. S. Samuelsen
Keyword(s):  
Natural Gas ◽  
Gas Turbine ◽  
Statistical Approach ◽  
Present System ◽  
Fuel Composition ◽  
Gas Turbine Combustor ◽  
Air Mixing ◽  
Gas Fuel ◽  
Model Gas Turbine Combustor ◽  
The Impact

In the area of stationary power generation, there exists a growing interest in understanding the role that gaseous fuel composition plays on the performance of natural gas-fired gas turbine systems. In this study, an atmospherically fired model gas turbine combustor with a fuel flexible fuel/air premixer is employed to investigate the impact of significant amounts of ethane and propane addition into a baseline natural gas fuel supply. The impacts of these various fuel compositions, in terms of the emissions of NOX and CO, and the coupled impact of the degree of fuel/air mixing, are captured explicitly for the present system by means of a statistically oriented testing methodology. These explicit expressions are also compared to emissions maps that encompass and expand beyond the statistically based test matrix to verify the validity of the employed statistical approach.

Development and Integration of the Dual Fuel Combustion System for the MGT Gas Turbine Family

2021 ◽  
Author(s):  
Bernhard Ćosić ◽  
Frank Reiss ◽  
Marc Blümer ◽  
Christian Frekers ◽  
Franklin Genin ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Distribution System ◽  
Gas Turbines ◽  
Liquid Fuel ◽  
Fuel Injection ◽  
Liquid Fuels ◽  
Dual Fuel ◽  
Gaseous Fuels ◽  
Supply And Distribution ◽  
Industrial Gas Turbines

Abstract Industrial gas turbines like the MGT6000 are often operated as power supply or as mechanical drives. In these applications, liquid fuels like 'Diesel Fuel No.2' can be used either as main fuel or as backup fuel if natural gas is not reliably available. The MAN Gas Turbines (MGT) operate with the Advanced Can Combustion (ACC) system, which is capable of ultra-low NOx emissions for gaseous fuels. This system has been further developed to provide dry dual fuel capability. In the present paper, we describe the design and detailed experimental validation process of the liquid fuel injection, and its integration into the gas turbine package. A central lance with an integrated two-stage nozzle is employed as a liquid pilot stage, enabling ignition and start-up of the engine on liquid fuel only. The pilot stage is continuously operated, whereas the bulk of the liquid fuel is injected through the premixed combustor stage. The premixed stage comprises a set of four decentralized nozzles based on fluidic oscillator atomizers, wherein atomization of the liquid fuel is achieved through self-induced oscillations. We present results illustrating the spray, hydrodynamic, and emission performance of the injectors. Extensive testing of the burner at atmospheric and full load high-pressure conditions has been performed, before verification within full engine tests. We show the design of the fuel supply and distribution system. Finally, we discuss the integration of the dual fuel system into the standard gas turbine package of the MGT6000.

scholarly journals Active Control Application to a Model Gas Turbine Combustor

1990 ◽  
Author(s):  
J. Brouwer ◽  
B. A. Ault ◽  
J. E. Bobrow ◽  
G. S. Samuelsen
Keyword(s):  
Feedback Control ◽  
Gas Turbine ◽  
Active Control ◽  
Input Parameter ◽  
Radiative Flux ◽  
Gas Turbine Combustor ◽  
Control Computer ◽  
Loop Feedback ◽  
Model Gas Turbine Combustor ◽  
Control Application

Closed-loop feedback control, developed in a axisymmetric can combustor, is demonstrated in a model can combustor with discrete wall jets. The study represents the initial steps toward the application of feedback control technology to practical gas turbine combustion systems. For the present application, the radiative flux from soot particulate is used as an indication of combustor performance, and nozzle atomizing air is selected as the input parameter. A measurement of radiative flux at the exit plane of the combustor is conveyed to a control computer which invokes an optimization algorithm to determine changes in the dome region necessary to minimize the radiative flux from soot. The results demonstrate the utility and potential of active control for maintaining optimal performance in real-time.

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