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Structural characteristics of nickel super alloy INCONEL 713LC after heat treatment

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Języki publikacji
EN
Abstrakty
EN
Purpose: Aircraft industry often uses nickel super-alloys for blades of jet engine turbines. This paper summarises analysis of infuence of heat treatment on structural characteristics of nickel super-alloy INCONEL 713C. Design/methodology/approach: Experimental investigation castings made of commercially produced nickel super-alloy INCONEL 713LC. Material was after heat treatment subjected to detailed structural analysis with use of methods of light microscopy (LM), or scanning electron microscopy (SEM) on microscopes OLYMPUS IX71 and JEOLJSM 50A. Findings: Mode of optimum heat treatment was proposed. On this basis of obtained results it is possible to recommend a heat treatment, which would consist of heating and dwell at the temperature exceeding 1240 degrees centigrade (min. 1260 degrees centigrade), so that precipitates at the grain boundaries dissolve completly, with subsequent slow cooling down to the temperature of approx. 940-950 degrees centigrade, so that there occurs intesive intra-granular precipitation of inter-metallic phase gamma'. Research limitations/implications: The experiment was limited by occurence a void in cast alloys. Practical implications: Aircraft industry often uses nickel super-alloys for blades of jet engine turbines. Originality/value: On the basis of obtained results it is possible to recommend the most suitable heat treatment, which produce intensive intra-granular precipitation of intermetallic phase gamma'. It was received a new know-how in this field.
Rocznik
Strony
29--32
Opis fizyczny
Bibliogr. 16 poz., fot., tab.
Twórcy
autor
autor
autor
autor
autor
  • VSB-Technical University of Ostrava, 17.listopadu 15, 708 33 Ostrava, Czech Republic, petr.jonsta@vsb.cz
Bibliografia
  • [1] V. Ustohal, Materials for Aircraft Industry, Textbook VUT Brno (1988) 130.
  • [2] http://www.tms.org/Meetings/Speciality/Superalloys2000/SuperalloysHistory.html
  • [3] http://wwvv.howitworks/gasturbine.com
  • [4] L. Swadźba, Mat. Conf. N-T, ENERGO-TECH-MAT, Ustroń. 1998.
  • [5] N. Saunders, et al. Modeling the Material Properties and Behavior of Ni-based Superalloys. In: Superalloys 2004. Eds.: A.K. GREEN, et al., TMS, Warendale (2004) 849.
  • [6] A.F. Souza, M.F. Bartos, M.R. Jorge, Thermal Engineering Vol. 3 (2004) 115.
  • [7] B. Formanek, S. Jóźwiak, B. Szczucka-Lasota, A. Dolata-Grosz, Z. Bojar, Intermetallic Alloys with Oxide Particles and Technological Concept for High Loaded Materials, Achievements in Mechanical and Materials Engineering, "AMME 2005", 235-242.
  • [8] B. Szczucka-Lasota, B. Formanek, L. Pajak, K. Szamański, Oxidation of HVOF Sprayed Coatings with NiAl Intermetallic Matrix and Ceramic Phases, Achievements in Mechanical and Materials Engineering, “AMME 2003”, 895-900.
  • [9] Z. Lekston, J. Drugacz, Structure and Properties of NiTi and TiNiCo Shape Memory Wires for Maxillofacial Surgery, Achievements in Mechanical and Materials Engineering, "AMME 2003", 593-596.
  • [10] G. Lojen, I. Anžel, A.C. Kneissl, A. Križman, E. Unterweger, B. Kosec, M. Bizjak, Microstructure of Rapid Solidified Cu-Al-Ni Shape Memory Alloy Ribbons, Achievements in Mechanical and Materials Engineering, "AMME 2005", 399-402.
  • [11] T. Podrábský, et al. Microstructural Changes of Turbine Wheel Made of the Alloy INCONEL 713LC. Mechanika No. 298/2004, Politechnika Opolska, 2004, 179.
  • [12] Y. KOIZUMI, T. KOBAYASHI, High Tem Mat. for Power Eng., II, Liege, 1998.
  • [13] L. Pajak, B. Formanek, G. Dercz, Dispersion Analysis of NiAl-TiC-Al203 Composite Powder, Achievements in Mechanical and Materials Engineering, "AMME 2003", 723-730.
  • [14] C.T. Sims, N.S. Stolaff, W.C. Hagel, Superalloys II. Wiley & Sons, New York, 1987.
  • [15] A. Hernas, Z. Jonšta, et al. Refractory Steels and Alloys ZUSI-Žilina, Slovakia, 2002.
  • [16] Z. Jonšta, Analysis of the Super-alloy INCONEL 713LC, Research Report, Ostrava, 2005.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BOS3-0016-0080
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