Abstract
Turbine engines need to be supplied both with fuel and oxygen contained in the air. The most important parameter of aviation fuel is its chemical composition, which decides the fuel’s operating properties.
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References
Kortylewski W (2008) Combustion and fuels. Wrocław University of Technolgy Press (in Polish)
Mrowiec P, Werber T (1975) Gas corrosion of metals. Śląsk Press, Katowice (in Polish)
Tubielewicz K, Melechow R (ed) (2003) Materials used in heat power engineering. Works of surface treatment team, Częstochowa (in Polish)
Chen X (2006) Calcium-magnesium-alumina-silicate (CMAS) delamination mechanisms in EB-PVD thermal barrier coatings. Surf Coat Technol 200:3418–3427
Eliaz N, Shemesh G, Latanision RM (2002) Hot corrosion in gas turbine components. Eng Fail Anal 9:32–43
Strangman T, Raybould D, Jameel A, Baker W (2007) Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils. Surf Coat Technol 202:658–664
Wellman R, Whitman G, Nicholls JR (2010) CMAS corrosion of EB PVD TBCs: identifying the minimum level to initiate damage. Int J Refract Metals Hard Mater 28:124–132
Wellman RG, Nicholas JR (2008) Erosion, corrosion and erosion–corrosion of EB PVD thermal barrier coatings. Tribol Int 41:657–662
Zschau HE, Dietrich M, Renusch D, Schutze M, Meijer J, Becker HW (2006) Detection of hydrogen in hidden and spalled layers of turbine blade coatings. Nucl Instrum Methods Phys Res B 249:381–383
Nicholls JR, Deakin MJ, Rickerby DP (1999) A comparison between the erosion behaviour of thermal spray and electron beam physical vapour deposition thermal barrier coatings. Wear 233–235:352–361
Johnson CA, Ruud JA, Bruce R, Wortman D (1998) Relationships between residual stress, microstructure and mechanical properties of electron beam–physical vapor deposition thermal barrier coatings. Surf Coat Technol 108–109:80–85
Kramer P, Yang J, Levi C (2006) Thermochemical interaction of thermal barrier coatings with CMAS deposits. J Am Ceram Soc 89:3167–3175
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
Steenbakker RJL, Wellman RG, Nicholas JR (2006) Erosion of gadolinia doped EB-PVD TBCs. Surf Coat Technol 201:2140–2146
Wellman RG, Deakin MJ, Nicholls JR (2005) The effect of TBC morphology and aging on the erosion rate of EB-PVD TBCs. Tribol Int 38:798–804
Chen X, He MY, Spitsberg I, Fleck NA, Hutchinson JW, Evans AG (2004) Mechanisms governing the high temperature erosion of thermal barrier coatings. Wear 256:735–746
Tassini N, Lambrinou K, Mircea I, Bartsch M, Patsias P, Van der Biest O (2007) Study of the amplitude-dependent mechanical behaviour of yttria-stabilised zirconia thermal barrier coatings. J Eur Ceram Soc 27:1487–1491
Crowell MW, Schaedler TA, Hazel BH, Konitzer DG, McMeeking RM, Evans AG (2012) Experiments and numerical simulations of single particle foreign object damage-like impacts of thermal barrier coatings. Int J Impact Eng 48:116–124
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Sadowski, T., Golewski, P. (2016). Environmental Loads. 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_5
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DOI: https://doi.org/10.1007/978-981-10-0919-8_5
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