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Technology of laser repair welding of nickel superalloy inner flaps of jet engine

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Purpose: of this paper: work out laser welding repair technology of cracked MIG 29 jet engine inner flaps made of cast nickel superalloy ŻS-3DK(ЖС-3ДК, Russian designation). Design/methodology/approach: The study were based on the analysis of laser HPDL powder INCONEL 625 welding of nickel superalloy using wide range of welding parameters to provide highest quality repair welds. Findings: Study of automatic welding technologies GTA, PTA and laser HPDL has shown that just laser welding can provide high quality repair welds. In order to establish the properties of welded joints repair cracks in the inner flap HPDL laser, studied the hardness, mechanical properties and erosive wear resistance. Research limitations/implications: It was found that only laser HPDL welding can provide high quality repair welds. Practical implications: The technology can be applied for repair cracked MIG 29 jet engine inner flaps. Originality/value: Repairing cracked MIG 29 jet engine inner flaps.
Rocznik
Strony
66--74
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
autor
  • Welding Department, Silesian University of Technology, ul. Konarskiego 18a, 44-100 Gliwice, Poland
  • Welding Department, Silesian University of Technology, ul. Konarskiego 18a, 44-100 Gliwice, Poland
Bibliografia
  • [1] L. Shepeleva, Laser cladding of turbine blades, Surface and Coatings Technology 125 (2000) 45-48.
  • [2] 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) 849-858.
  • [3] A. Gillner, Laser applications in microtechnology, Journal of Materials Processing Technology 167 (2005) 494-498.
  • [4] Pratt & Whitney Canada Corporation Specification, Micro -weld repair of turbine vane and vane segment castings.
  • [5] S. Nowotny, S. Scharek, A. Schmidt, Advanced laser technology applied to cladding and buildup welding Journal, 5 (2007).
  • [6] A. Klimpel, A. Olejnik, D. Janicki, A. Lisiecki, Investigations of technology of repair laser welding of exhaust flaps of jet engine made of nickel superalloy, Welding Technology Review 12 (2009) 3-7 (in Polish).
  • [7] D.J. Tillack, Welding superalloys for aerospace applications, Superalloys, Welding Journal (2007) 30-38.
  • [8] R.F. Singer, Advanced materials and processes for land based gas turbines, Materials for advanced power engineering, Part. II, Proceedings of the Conference, Edited by D. Coutsouradis, Liege, Belgium (1994) 1720.
  • [9] L. Swadźba, Erosion and corrosion resistant coatings for aircraft compressor blades, Surface and Coatings Technology 62 (1993) 486-492.
  • [10] I.A. Choudhury, M.A. El-Baradie, Machinability of nickelbase super alloys: a general review, Journal of Materials Processing Technology 77 (1998) 15-24.
  • [11] M. Zielińska, M. Yavorska, M. Poręba, J. Sieniawski, Thermal properties of cast nickel based superalloys, Archives of Materials Science and Engineering 44/1 (2010) 35-38.
  • [12] S.A. Sajjadi, S.M. Zebarjad, Effect of temperature on tensile fracture mechanisms of a Ni-base superalloy, Archives of Materials Science and Engineering 28/1 (2007) 34-40.
  • [13] M. Hetmańczyk, L. Swadźba, B. Mendala, Advanced materials and protective coating in aero-engines application, Journal of Achievements in Materials and Manufacturing Engineering 24/1 (2007) 372-381.
  • [14] Z. Jonšta, J. Sojka, A. Hernas, Strucutral characteristics of nickel super alloy INCONEL 713LC after heat treatment, Journal of Achievement in Materials and Manufacturing Engineering 21 (2007) 33-36.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-4c35bff4-f2e4-45a5-873f-184e9909088f
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