Gas Turbine Aero-Engines

  • Stefano Gialanella
  • Alessio Malandruccolo
Part of the Topics in Mining, Metallurgy and Materials Engineering book series (TMMME)


In this chapter the main structural aspects and working principles of the gas turbine aero-engines are recalled, with the main aim to highlight the most interesting properties of the materials used for the main components of these engines. Over the years, the new requirements for better performing gas turbine aero-engines have been sustained by the availability of novel materials. The last section is specifically dedicated to the latest developments in aerospace gas turbine engines, in order to highlight the future trends and guidelines on which materials research efforts are concentrated.


  1. Boyce M P (2012) Gas Turbine Engineering Handbook 4th edn. Elsevier, OxfordGoogle Scholar
  2. Cumpsty N (2003) Jet Propulsion: A Simple Guide to Aerodynamic and Thermodynamic Design and Performance of Jet Engine 2nd edn. Cambridge University PressGoogle Scholar
  3. European Commission (2011) Flightpath 2050 Europe’s Vision for Aviation. Available via DIALOG. Accessed 17 Aug 2017
  4. European Commission (2016) European Aviation Environmental Report 2016. Available via DIALOG. Accessed 17 Aug 2017
  5. Giampaolo A (2006) Gas Turbine Handbook Principles and Practices. The Fairmont Press Inc., LilburnGoogle Scholar
  6. Gunston B (1995) The Development of Jet and Turbine Aero Engines. Patrick Stephens Ltd PublGoogle Scholar
  7. Kear B H (1986) Advanced Metals. Scientific American 220: 130–139Google Scholar
  8. Martin R (2016) The Race for the Ultra-Efficient Jet Engine of the Future. In: Sustainable Energy. MIT Technology Review. Accessed 15 Aug 2017
  9. Meetham G W (1981) The Development of Gas Turbine Materials. Applied Science Publishers Ltd, LondonCrossRefGoogle Scholar
  10. MTU Aero Engines (2016) GP7000 turbofan engine. Available via Dialog. Accessed 07 Sept 2017
  11. Mukherji D et al (2011) Beyond Ni-based Superalloys: Development of CoRe-based Alloys for Gas Turbine Applications at Very High Temperatures. International Journal of Materials Research 102(9): 1125–1132CrossRefGoogle Scholar
  12. Pratt & Whitney (2012) F135 Specs Charts. Available via DIALOG. Accessed 06 Sept 2017
  13. Reed R C (2006) The Superalloys-Fundamentals and Applications. Cambridge University Press, New YorkCrossRefGoogle Scholar
  14. Rolls-Royce (1996) The Jet Engine 5th edn. Rolls-Royce plc, DerbyGoogle Scholar
  15. Rolls-Royce (2015) Trent 900. Available via DIALOG. Accessed 07 Sept 2017
  16. Rolls-Royce (2016) Trent XWB. Available via DIALOG. Accessed 17 Aug 2017
  17. Rolls-Royce (2017) Pioneering intelligent innovation for our customers. Accessed 23 Aug 2017
  18. The Washington Post (2017) The next generation of eco-friendly airplanes has arrived…quietly. Accessed 17 Aug 2017
  19. Wenger U (2014) Rolls-Royce Technology for the Future Aircraft Engines. Lecture for RAeS, DGLR, VDI at the Hamburg University of Applied Sciences, Hamburg, 20 March 2014Google Scholar

Further Reading

  1. Connors J (2010) The Engines of Pratt & Whitney. American Institute of Aeronautics and Astronautics, Inc.Google Scholar
  2. Hill P G, Peterson C R (1992) Mechanics and Thermodynamics of Propulsion 2nd edn. PearsonGoogle Scholar
  3. Kerrebrock J L (1992) Aircraft Engines and Gas Turbines 2nd edn. The MIT PressGoogle Scholar
  4. Soares C (2015) Gas Turbines: A Handbook of Air, Land and Sea Applications. ElsevierGoogle Scholar

Copyright information

© Springer Nature Switzerland AG 2020

Authors and Affiliations

  • Stefano Gialanella
    • 1
  • Alessio Malandruccolo
    • 2
  1. 1.Industrial Engineering DepartmentUniversity of TrentoTrentoItaly
  2. 2.Metallurgy Industrial ConsultantBolzanoItaly

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