Skip to main content Accessibility help
×
Hostname: page-component-848d4c4894-r5zm4 Total loading time: 0 Render date: 2024-06-22T23:55:50.739Z Has data issue: false hasContentIssue false

10 - Industrial Combustors

Conventional, Non-premixed, and Dry Low Emissions (DLN)

from Part 3 - Case Studies and Specific Technologies: Pollutant Trends and Key Drivers

Published online by Cambridge University Press:  05 June 2013

Tim C. Lieuwen
Affiliation:
Georgia Institute of Technology
Vigor Yang
Affiliation:
Georgia Institute of Technology
Get access

Summary

Introduction

Modern industrial gas turbine combustors have to meet a wide range of technical requirements governed by the thermodynamic cycle, the demand for a low environmental impact, the compatibility with other machine components, and the safety and reliability aspects. Although the evolution of combustion chamber technology has resulted in substantially different hardware solutions, a high level of similarity exists as to how the subprocesses take place in combustion chambers of different design and how they interact with each other. What the basic designs of combustors for industrial gas turbines relevant to emissions have in common will be discussed in the first part of this chapter to create the basis for a better understanding of the second part, where several specific design solutions are presented. These are grouped into different classes of combustors according to fuel type and the pollutant emission abatement technique employed. The present state of the art is the result of the simultaneous optimization of several subprocesses relevant for the performance of combustors. Expanded discussion of many of the basic combustor technology drivers and how they interact with the electrical grid as a whole, the power plant, and the gas turbine are also included in Chapter 1.

Beyond Energy Conversion

Taking the thermodynamic cycle of gas turbines into consideration, the main function of the combustor is to provide a high-temperature fluid flow for driving the subsequent turbine. For older gas turbine designs dating from before 1980, the requirements of the gas turbine combustion system were quite moderate and so the development effort was kept low. Pollutant emissions were of only peripheral concern, as long as soot and yellow smoke from nitrogen dioxide formation were below the limits of visibility. These requirements were met using fairly simple combustors, which were easy to operate without sophisticated control and periphery. Because of the enormous increase of turbine inlet temperatures in high-efficiency gas turbines and the stricter emissions regulations, the design of combustors for gas turbines has become a key technology. Since 1980, the abatement of pollutant emissions has entirely driven combustor development for industrial gas turbines. This has led to the more complex and delicate multi-burner systems, which are the state of the art today.

Type
Chapter
Information
Gas Turbine Emissions , pp. 290 - 362
Publisher: Cambridge University Press
Print publication year: 2013

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Aoyama, K. et al. (1991). “Development of a Dry Low NOx Combustor for a 120MW Gas Turbine.” Proceedings of the ASME/IGTI TurboExpo, Paper ASME 91-GT-297.
Bailey, J. C., Intile, J., Fric, T. F., Tolpadi, A. K., Nirmalan, N. V., and Bunker, R. S. (2002). “Experimental and Numerical Study of Heat Transfer in a Gas Turbine Combustor Liner.” Proceedings of the ASME/IGTI TurboExpo, Paper 2002-GT-3018.CrossRef
Bland, R., Ryan, W., Abou-Jaoude, K., Bandatu, R., Haris, A., and Rising, B. (2004). “Siemens W501F Gas Turbine: Ultra Low NOx Combustion System Development.” Proceedings of the Power-Gen International.Google Scholar
Bradley, D. (1992). “How Fast Can We Burn?” Twenty-fourth Symposium (International) on Combustion, 247–62.CrossRef
Davis, B. (1996). “Dry Low-NOx Combustion Systems for GE Heavy-Duty Gas Turbines.” Proceedings of the ASME/IGTI TurboExpo, Paper 96-GT-27.
Dean, A. M., and Bozzelli, J. W. (2000). “Combustion Chemistry of Nitrogen,” in Gas-Phase Combustion Chemistry, Gardiner W. C. ed., Springer-Verlag.CrossRefGoogle Scholar
Döbbeling, K., Pacholleck, J., and Hoffs, A. (2007). “Combining Operational Flexibility with Clean, Reliable Power Generation in the Alstom Gas Turbine GT13E2.” Proceedings of the Power-Gen Asia Conference.
Eroglu, A., Döbbeling, K., Joos, F., and Brunner, P. (2001). “Vortex Generators in Lean-Premix Combustion.” Transactions of the ASME, Journal of Engineering for Gas Turbines and Power 123: 41–9.CrossRefGoogle Scholar
Eroglu, A., Flohr, P., Brunner, P., and Hellat, J. (2009). “Combustor Design for Low Emissions and Long Lifetime Requirements.” Proceedings of the ASME/IGTI TurboExpo, Paper GT2009–59540.CrossRef
Gruschka, U. et al. (2008). “ULN System for the New SGT5–8000H Gas Turbine: Design and High Pressure Rig Test Results.” Proceedings of the ASME/IGTI TurboExpo, Paper No. GT2008–51208.CrossRef
Hall, J. M., Thatcher, R. T., Koshevets, S., Thomas, L. L., and Jones, R. M. (2011). “Development and Field Validation of a Large-Frame Gas Turbine Power Train for Steel Mill Gases.” Proceedings of the ASME/IGTI TurboExpo, Paper GT2011–45923.CrossRef
Johnson, C. et al. (2008). “Ultra Low NOx Combustion Technology.” Proceedings of the Power-Gen International.
Joos, F., Brunner, P., Schulte-Werning, B., Syed, K., and Eroglu, A. (1996). “Development of the Sequential Combustion System for the ABB GT24/GT26 Gas Turbine Family.” Proceedings of the ASME/IGTI TurboExpo, Paper 1996-GT-315.CrossRef
Kalb, J. R., and Sattelmayer, T. (2006). “Lean Blowout Limit and NOx Production of a Premixed Sub-ppm NOx Burner with Periodic Recirculation of Combustion Products.” Journal of Engineering for Gas Turbines and Power 128: 247–54.CrossRefGoogle Scholar
Kenyon, M., and Fluck, M. (2005). “Using Non Standard Fuels in the ALSTOM GT11N2 Gas Turbine.” Proceedings of the Power-Gen International.
Krebs, W., Walz, G., Judith, H., and Hoffmann, S. (1999). “Detailed Analysis of the Thermal Wall Heat Transfer in Annular Combustors.” Proceedings of the ASME/IGTI TurboExpo, Paper 99-GT-134.
Lewis, S., Thomas, S. R., Joseph Citeno, J., and Natarajan, J. (2011). “F-Class DLN Technology Advancements: DLN2.6+.” Proceedings of the ASME/IGTI TurboExpo, Paper GT2011–45373.
Lovett, J. A., and Abuaf, N. (1992). “Emissions and Stability Characteristics of Flameholders for Lean-Premixed Combustion.” Proceedings of the ASME/IGTI TurboExpo, Paper 92-GT-120.CrossRef
Lovett, J. A., and Mick, W. (1995). “Development of a Swirl and Bluff-Body Stabilized Burner for Low-NOx, Lean-Premixed Combustion.” Proceedings of theASME/IGTI TurboExpo, Paper 95-GT-168.CrossRef
Matsuzaki, H. et al. (1984). “Investigation of Combustion Structure Inside Low NOx Combustors for a 1500C-class Gas Turbine.” Transactions of the ASME, Journal of Engineering for Gas Turbine and Power 106: 795–800.Google Scholar
Payrhuber, K., Jones, R. M., Scholz, M. H. (2008). “Gas Turbine Flexibility with Carbon Constrained Fuels.” Proceedings of the ASME/IGTI TurboExpo, Paper GT2008–50556.CrossRef
Reiss, F., Griffin, T., and Reyser, K. (2002). “The ALSTOM GT13E2 Medium Btu Gas Turbine.” Proceedings of the ASME/IGTI TurboExpo, Paper GT 2002 30108.CrossRef
Sattelmayer, T., Felchlin, M. P., Haumann, J., Hellat, J., Styner, D. (1992). “Second Generation Low-Emission Combustors for ABB Gas Turbines: Burner Development and Tests at Atmospheric Pressure.” Transactions of the ASME, Journal of Engineering for Gas Turbine and Power 114(1): 118–25.CrossRefGoogle Scholar
Sattelmayer, T., Polifke, W., Winkler, D., and Döbbeling, K. (1998). “NOx-Abatement Potential of Lean-Premixed GT-Combustors.” Transactions of the ASME, Journal of Engineering for Gas Turbine and Power 120: 48–59.CrossRefGoogle Scholar
Senior, P., Lutum, E., Polifke, W., and Sattelmayer, T. (1993). “Combustion Technology of the ABB GT13E2 Annular Combustor.” Proceedings of the Twentieth CIMAC Conference, Paper G22.
Streb, H., and Prade, B. (2001). “Advanced Burner Development for the Vx4.3A Gas Turbines.” Proceedings of ASME IGTI TurboExpo, Paper 2001-GT-0077.
Thomas, L. L., Simons, D. W., Popovic, P., Romoser, C. E., Vandale, D. D., and Citeno, J. V. (2011). “E-Class DLN Technology Advancements, DLN1+.” Proceedings of the ASME/IGTI TurboExpo, Paper GT2011–45944.CrossRef
Vandervort, C. L. (2000). “9 ppm NOx / CO Combustion System for ‘F’ Class Industrial Gas Turbines.” Proceedings of the ASME/IGTI TurboExpo, Paper 2000-GT-0086.CrossRef

Save book to Kindle

To save this book to your Kindle, first ensure coreplatform@cambridge.org is added to your Approved Personal Document E-mail List under your Personal Document Settings on the Manage Your Content and Devices page of your Amazon account. Then enter the ‘name’ part of your Kindle email address below. Find out more about saving to your Kindle.

Note you can select to save to either the @free.kindle.com or @kindle.com variations. ‘@free.kindle.com’ emails are free but can only be saved to your device when it is connected to wi-fi. ‘@kindle.com’ emails can be delivered even when you are not connected to wi-fi, but note that service fees apply.

Find out more about the Kindle Personal Document Service.

Available formats
×

Save book to Dropbox

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Dropbox.

Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

Available formats
×