Czasopismo
2006
|
Vol. 17, nr 1-2
|
177--180
Tytuł artykułu
Autorzy
Wybrane pełne teksty z tego czasopisma
Warianty tytułu
Języki publikacji
Abstrakty
Purpose: The paper presents the evaluation of the influence of aluminium layers used as protective coatings of aircraft turbine engine blades upon durability of ŻS6U nickel base superalloy under the conditions of short time creep. The conditions of cracks formation and growth in specimens with aluminium coatings have been analysed while taking into account the microstructure properties of coatings as well as the microstructure of specimen core material. Design/methodology/approach: The creep tests have been performed on MTS apparatus in the conditions corresponding to the extreme operating conditions of aircraft engine blades. The specimens were heated in a resistance furnace up to the temperature of 950ºC and then constant axial force was applied which induced stress σo=300 MPa in their cross-section. Findings: The obtained results have proved a significant influence of the type, protective coating thickness and the specimen core structure upon the secondary creep rate. Research limitations/implications: To ensure the most effective use of aluminium protective coatings it is important to understand the creep mechanisms in temperature lower than DBTT (ductile brittle transition temperature). Therefore, it is necessary to perform some creep tests in temperatures much lower than 900ºC. Practical implications: The obtained results could constitute the base for suggesting the guidelines on selecting proper aluminium coatings for specific designs of aircraft engine blades. Originality/value: It has been found that the reduction of creep durability of specimens made of ŻS6U alloy with diffusive aluminium coatings is caused by the reduction of the lateral surface of specimens core, which effectively transfers loads in creep tests.
Rocznik
Tom
Strony
177--180
Opis fizyczny
Bibliogr. 15 poz., rys., tab., wykr.
Twórcy
autor
- Department of Material Engineering and Metallurgy, Silesian University of Technology, 40 019 Katowice, ul. Krasińskiego 8, Poland, marek.ciesla@polsl.pl
autor
- Department of Material Engineering and Metallurgy, Silesian University of Technology, 40 019 Katowice, ul. Krasińskiego 8, Poland
Bibliografia
- [1] Superalloys II, edited by T. Sims, W. Hagel, S. Stoloff, Interscience Publication J. Wiley & Sons, 1987, chapter 2, 27-56.
- [2] J. Sieniawski, Criteria and methods of evaluation of materials for parts of aircraft turbine engines, Oficyna Wydawnicza Pol. Rzeszowskiej, 1995, (in Polish)
- [3] L. Swadźba, A. Maciejny, B. Mendala, G. Moskal, Structure and resistance to oxidation of an Al-Si diffusion coating deposited by Arc-PVD on a TiAlCrNb alloy, Surface and Coatings Technology 165, 2003, 273-280.
- [4] D.K. Das, V. Singh, S.V. Joshi, Evolution of aluminide coating microstructure on nickel-base cast superalloy CM-247 in a single-step high-activity aluminizing process, Metallurgical and Materials Transaction A, vol.29A, Aug. 1998, 2173-2188.
- [5] L. Swadźba, B. Mendala, M. Hetmańczyk, Degradation of aluminide, chromium-aluminide and thermal barrier coatings in conditions of cyclic thermal and mechanical loads, European Federation of Corrosion Pub., 27, Frankfurt/Main, 1999, 392-406.
- [6] Y. Tamarin, Protective coatings for turbine blades, ASM International, The Materials Information Society, Materials Park, Ohio 44073-2002, 55-78.
- [7] J. Okrajni, M. Cieśla, L. Swadźba, High-temperature low-cycle fatigue and creep behaviour of nickel-based super-alloys with heat-resistant coatings, Fatigue and Fractute of Materials and Engineering Structures, 1998; 21, 947-954.
- [8] G. W. Goward, Progress in coatings for gas turbine airfoils, Surface and Coating Technology 108-109, 1999, 73-79.
- [9] H. W. Grunling, H. Rechtenbacher, L. Singheiser, Some practical aspects of corrosion and coatings in utility gas turbines, Material Science Forum, Vols. 251-254, 1997, 483-502.
- [10] J. R. Nicholls, Designing oxidation-resistant coatings, JOM, January 2000, 28-35.
- [11] J. Wyrzykowski, E. Pleszakow, J. Sieniawski, Deformation and cracking of metals, WNT Warszawa 1999, (in Polish).
- [12] D. Locq, M. Marty, P. Caron, Optimisation of the mechanical properties of a new PM superalloy for disk applications, Superalloys 2000, ed. T.M. Pollock et al, TMS 2000, 395-403.
- [13] U. Tetzlaff and H. Mughrabi, Enhancement of the high-temperature tensile creep strength of monocrystalline nickel-base superalloys by pre-rafting in compression, Superalloys 2000, ed. T.M. Pollock et al, TMS 2000, 273-281.
- [14] I. M. Wilcock, P. Lukas, M. Maldini, J. Klabbers, B. Dubiel and M. B. Henderson, The creep behaviour of AS-CAST SX CM186LC at industrial gas turbine Materials for Advanced Power Engineering 2002, ed. J. Lecomte-Beckers et al, Proceedings of the 7th Liege Conference, Part I, 139-148.
- [15] T.P. Gaab, S.L. Draper, D.R. Hull, R.A. MacKay and M.V. Nathal, The role of interfacial dislocation networks in High temperature Creep of superalloys, Materials Science and Engineering, A 118 (1989), 59-69.
Typ dokumentu
Bibliografia
Identyfikatory
Identyfikator YADDA
bwmeta1.element.baztech-1886f7bb-79ab-4d94-8d04-df27dbff96f6