Skip to main content

Modeling of Recuperators, Combustion Chambers, Afterburners

  • Chapter
  • First Online:
Gas Turbine Design, Components and System Design Integration
  • 1045 Accesses

Abstract

This category of components includes recuperators, preheaters, regenerators, intercoolers, and aftercoolers, Figure 14.1 Within these components the process of heat exchange occurs between the high and low temperature sides. The working principle of these components is the same ([1, 2, 2]). However, different working media are involved in the heat transfer process. More recently recuperators are applied to small and medium size gas turbine engines to improve their thermal efficiency. The exhaust thermal energy is used to warm up the compressor exit air before it enters the combustion chamber. A typical recuperator consists of a low pressure hot side flow path, a high pressure cold side flow path, and the wall that separates the two flow paths. A variety of design concepts are used to maximize the heat exchange between the hot and the cold side by improving the heat transfer coefficients. A cold side flow path may consist of a number of tubes with turbulators, fin pins, and other features that enhance the heat transfer coefficient. Based on the individual recuperator design concept, hot gas impinges on the tube surface in cross flow or counter flow directions. The working media entering and exiting the recuperator is generally combustion gas that exits the diffuser (hot side) and air that exits the compressor (cold side)

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 219.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Hardcover Book
USD 279.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Bibliography

  1. Schobeiri T., 1986: “A General Computational Method for Simulation and Prediction of Transient Behavior of Gas Turbines,” ASME-86-GT-180.

    Google Scholar 

  2. Schobeiri, M. T., Abouelkheir, M., Lippke, C., 1994, “GETRAN: A Generic, Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero-and Power Generation Gas Turbine Engines,” an honor paper, ASME Transactions, Journal of Gas Turbine and Power, Vol. 1, pp. 483–494.

    Article  Google Scholar 

  3. Schobeiri, M. T., Attia, M, Lippke, C., 1994, “Nonlinear Dynamic Simulation of Single and Multi-spool Core Engines, Part I, II: Theoretical Method, Simulation Cases” AIAA, Journal of Propulsion and Power, Volume 10, Number 6, pp. 855–867, 1994.

    Article  ADS  Google Scholar 

  4. Kays, W. M, London, A. L., 1984, “Compact Heat Exchangers,” McGraw-Hill Book Company, third Edition.

    Google Scholar 

  5. Hansen, H., 1976, “Wärmeübertragung im Gegenstrom, Gleichstrom und Kreuzstrom, 2.” Auflage, ISBN 3ß540ß07552ß6 Springer-Verlag, Berlin Heidelberg New York.

    Google Scholar 

  6. Lefebvre, AS.H ., 1983, “Gas Turbine Combustion,” Hemisphere Publishing Corporation.

    Google Scholar 

  7. Marek, C. J., and Huhasz, A. J., 1974, “Simulataneous Film and Convection Cooling of a Plate inserted in the Exhaust Stream of a Gas Turbine Combustor,” NASA TND-7689.

    Google Scholar 

  8. Planck, M., 1959, “Theory of Heat Radiation,” Dover Publication, Inc, New York.

    MATH  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Meinhard T. Schobeiri .

Rights and permissions

Reprints and permissions

Copyright information

© 2019 Springer Nature Switzerland AG

About this chapter

Check for updates. Verify currency and authenticity via CrossMark

Cite this chapter

Schobeiri, M.T. (2019). Modeling of Recuperators, Combustion Chambers, Afterburners. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-030-23973-2_14

Download citation

Publish with us

Policies and ethics