Skip to main content

Protective Thermal Barrier Coatings

  • Chapter
  • First Online:

Part of the book series: SpringerBriefs in Applied Sciences and Technology ((BRIEFSCOMPUTAT))

Abstract

The goal of using TBCs is, e.g. to reduce thermal conductivity between exhaust gases and the blade material, anti-corrosion protection and increased wear resistance.

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

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   39.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   54.99
Price excludes VAT (USA)
  • Compact, lightweight 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

Learn about institutional subscriptions

References

  1. Hongbo G, Hongju Z, Guohui M, Shengkai G (2009) Thermo-physical and thermal cycling properties of plasma sprayed BaLa2Ti3O10 coating as potential thermal barrier materials. Surf Coat Technol 204:691–696

    Google Scholar 

  2. Liu ZG, Ouyang JH, Zhou Y (2009) Heat capacities and derived thermodynamic functions of neodymium–gadolinium zirconates from 298.15 to 1050 K. J Alloys and Compd 475:21–24

    Google Scholar 

  3. Fenech J, Dalbin M, Barnabe A, Bonino JP, Ansart F (2001) Sol–gel processing and characterization of (RE-Y)-zirconia powders for thermal barrier coatings. Powder Technol 208:480–487

    Google Scholar 

  4. Hongming Z, Danqing Y (2008) Effect of rare earth doping on thermo-physical properties of lanthanum zirconate ceramic for thermal barrier coatings. J Rare Earths 26:770–774

    Google Scholar 

  5. Hongsong Z, Kun P, Qiang X, Fuchi W, Ling L (2009) Thermal conductivity of (Sm1−xLax)2Zr2O7 (x = 0, 0.25, 0.5, 0.75 and 1) oxides for advanced thermal barrier coatings. J Rare Earths 27:222

    Google Scholar 

  6. Ma W, Dong H, Guo H, Gong P, Zheng X (2010) Thermal cycling behavior of La2Ce2O7/8YSZ double-ceramic-layer thermal barrier coatings prepared by atmospheric plasma spraying. Surf Coat Technol 204:3366–3370

    Google Scholar 

  7. Ma W, Macka D, Malzbender J, Vaßen R, Stover D (2008) Yb2O3 and Gd2O3 doped strontium zirconate for thermal barrier coatings. J Eur Ceramic Soc 28:3071–3081

    Google Scholar 

  8. Maekawa T, Kurosaki K, Yamanaka P (2007) Thermophysical properties of BaY2O4: A new candidate material for thermal barrier coatings. Mater Lett 61:2303–2306

    Google Scholar 

  9. Ramachandran CP, Balasubramanian V, Ananthapadmanabhan PV (2012) Synthesis, spheroidization and spray deposition of lanthanum zirconate using thermal plasma process. Surf Coat Technol 206:3017–3035

    Google Scholar 

  10. Tamura M, Takahashi M, Ishii J, Suzuki K, Sato M, Shimomura K (1999) Multilayered thermal barrier coating for land-based gas turbines. J Therm Spray Technol 8:68–72

    Google Scholar 

  11. Wan C, Qu Z, Du A, Pan W (2009) Influence of B site substituent Ti on the structure and thermophysical properties of A2B2O7-type pyrochlore Gd2Zr2O7. Acta Materialia 57:4782–4789

    Google Scholar 

  12. Xie X, Guoa H, Gonga P, Xua H (2011) Lanthanum–titanium–aluminum oxide: a novel thermal barrier coating material for applications at 1300 °C. J Eur Ceramic Soc 31:1677–1683

    Google Scholar 

  13. Niezgoda T, Małachowski J, Szymczyk W (2005) Numerical modelling of ceramic microstructure. WNT, Warszawa (in Polish)

    Google Scholar 

  14. Chen JP, Duh JG (2001) Indentation behavior and Young’s modulus evaluation in electroless Ni modified CrN coating on mild steel. Surf Coat Technol 139:6–13

    Google Scholar 

  15. Chen X, Hutchinson JW (2002) Particle impact on metal substrates with application to foreign object damage to aircraft engines. J Mech Phys Solids 50:2669–2690

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Tomasz Sadowski .

Rights and permissions

Reprints and permissions

Copyright information

© 2016 The Author(s)

About this chapter

Cite this chapter

Sadowski, T., Golewski, P. (2016). Protective Thermal Barrier Coatings. In: Loadings in Thermal Barrier Coatings of Jet Engine Turbine Blades. SpringerBriefs in Applied Sciences and Technology(). Springer, Singapore. https://doi.org/10.1007/978-981-10-0919-8_2

Download citation

  • DOI: https://doi.org/10.1007/978-981-10-0919-8_2

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-0918-1

  • Online ISBN: 978-981-10-0919-8

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics