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Tytuł artykułu

Simulation and bench studies of the constructively and technologically modernized high performance piston aircraft engine. Stage I

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents an analysis of tribological wear of an assembly composed of cylinder liner and piston rings in a piston aircraft engine. In place of the previously used technology of gas nitriding of the cylinder liner (made out of 38CrAlMo6‒10 steel), formation of multi-component or composite layers by nitriding in plasma discharge environment was proposed. Also, a modification of the previously used chromium coating of the piston rings by plasma nitriding was proposed. A study on the structure and properties of surface layer diffusion manufactured by utilizing the phenomenon of cathode sputtering was carried out. Wear resistance tests were performed on a specially designed bench, with the use of isotope markers. Verification of each of the friction couples was based on using the wear of the ring as a function of the distance trip, and the roughness of the cylinder liner and ring.
Słowa kluczowe
EN
PL
Rocznik
Strony
93--105
Opis fizyczny
Bibliogr. 12 poz., tab., rys., wykr.
Twórcy
autor
  • Institute of Machine Design Fundamentals, Warsaw University of Technology, 84 Narbutta St., 02-524 Warsaw, Poland
  • Faculty of Materials Science and Engineering, Warsaw University of Technology, 141 Wołoska St., 02-507 Warsaw, Poland
autor
  • Faculty of Materials Science and Engineering, Warsaw University of Technology, 141 Wołoska St., 02-507 Warsaw, Poland
autor
  • Institute of Machine Design Fundamentals, Warsaw University of Technology, 84 Narbutta St., 02-524 Warsaw, Poland
Bibliografia
  • [1] W. Ostapski, “Analysis of thermo-mechanical response in an aircraft piston engine by analytical, FEM, and test-stand investigations”, Journal of Thermal Stresses 34, 285-312 (2011).
  • [2] W. Ostapski, “Raport projektu celowego nr 6 T08 154 2001C/5673: Wdrożenie technologii wytwarzania kompozytowych, dyfuzyjnych warstw przeciwzużyciowych w produkcji elementów silników lotniczych” 2002-2005, 2006, [in Polish].
  • [3] T. Burakowski and T. Wierzchoń, Surface Engineering of Metals: Principles, Equipment, Technologies, CRC Press, New York, 1999.
  • [4] T. Wierzchoń, J. Rudnicki, M. Hering, and R. Niedbała, “Formation and properties of nitrided layers produced in pulsed plasma at a frequency between 10 and 60 kHz”, Vacuum 48 (6) 499-502 (1997).
  • [5] T. Wierzchoń, “Structure and properties of multicomponent and composite layers produced by combined surface engineering methods”, Surface and Coatings Technology 180-181, 458-464 (2004).
  • [6] M. Tacikowski, I. Ulbin-Pokorska, and T. Wierzchoń, “Microstructure of the composite oxynitrided chromium layers produced on steel by a duplex method”, Surface and Coatings Technology 201, 2776-2781(2006)
  • [7] PN-83 H-04302, “Badania wytrzymałościowe metali. Próba tarcia w układzie: 3 wałeczki-stożek”, [in Polish].
  • [8] A. Jarkiewicz, E. Roliński, and T. Wierzchoń, “Experimental determination of influence of residual stresses on thermochemical processes in tool steels”, Materials Science and Technology 2, 635-629 (1986)
  • [10] W. Ostapski, “Introductory analysis of causes of decreasing operating of Asz-62IR aircraft engine”, IX Polish-Ukrainian Conf. on “CAD in Machinery Design”, Poland, 109-120 (2001).
  • [11] W. Ostapski, “Test stand examinations and analysis of wear in aircraft piston engines”, Proc. VI Conf. The Control of Fluid Systems, Slovakia, (2001).
  • [12] W. Ostapski, “Optimization of surface layer parameters of frictional pair ring-cylinder bearing surface of ASz-62IR aircraft engine with regard to abrasive wear criterion”, IX Polish-Ukrainian Conf. on “CAD in Machinery Design”, Poland, 121-130 (2001).
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6fdc1445-850c-4289-b43b-71228d18d022
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