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          charges, as well as the parameters of the coating spraying process, on the formation of
          the structure, phase composition and wear resistance of the coatings under conditions of
          boundary lubrication during friction and abrasive wear were used as a guideline.
               The process of creating hard anodised layers on aluminium alloys has been updated
          by incorporating hydrogen peroxide (30-50 mg/l) into the electrolyte solution, which is
          composed of 20% sulfuric acid. Another method involves the use of ozone gas during the
          synthesis process. The use of this material has allowed for significant improvements in
          several key areas. The thickness of the anodized layer has been increased by 50-60%,
          microhardness has been boosted by 40-50%, abrasive wear resistance has been enhanced
          by 15%, and wear resistance in a friction pair with a steel ball has been increased by 30%.
               We have developed a method for pulsed hard anodising of aluminium alloys. This
          method  allows  one  phase  or  a  mixture  of  two  phases  to  form  in  the  structure  of  the
          anodised  layer  (depending  on  the  electrolyte  temperature  (–5…+5)°C)  during  the
          synthesis  process.  The  Al₂O₃•H₂O  (boehmite)  phase  in  the  microstructure  of  the
          anodised  layers  provides  high  microhardness  and  abrasive  wear  resistance,  while  the
          Al₂O₃•3H₂O (hibinite) phase provides high tribological properties. The anodised layer
          obtained using the pulse method was 15–20% thicker and had 1.5–3 times greater wear
          resistance than layers anodised using stationary synthesis, and 2.5–8 times greater wear
          resistance than the D16 alloy.
               It  was  shown  that  during  the  synthesis  of  PEO  layers  on  top  of  thermal  spray
          coatings of the Al-Mg, Al-Ni, Al-Cu, Al-Ti systems, low-melting and fluid eutectics are
          formed from mixtures of oxides (Al 2O 3 + MgO), (Al 2O 3 + NiO), (Al 2O 3 + CuO), (Al 2O 3
          + TiO 2), which fill discharge channels more easily than the refractory oxide Al 2O 3. This
          made  it  possible  to  reduce  the  porosity  of  the  synthesized  PEO  layer  (from  8...10  to
          3...5%), increase the corundum content in it (from 30 to 70%), increase its microhardness
          (by 300...500 HV 0.3) and abrasive wear resistance (by 4...6 times). The wear mechanism
          of different types of counterbodies (made of cast iron, bronze, babbitt and steel) during
          their  frictional  interaction  with  the  PEO  layer  was  established.  With  a  counterbodies
          hardness  of up to 300 HV 0.3, wear occurred  due to the  removal of the layer from  the
          counterbodied surface by protrusions on the PEO layer as cutters. Such a friction pair is
          suitable  for  use  only  at  specific  loads  up  to  4  MPa.  At  a  counterbody  hardness  of
          (300…1000) HV 0.3, wear occurred due to multiple elastic or elastic-plastic deformation of
          the counterbody surface. Such a friction pair is suitable for use at specific loads up to
          10 MPa.
               A  method  for supersonic arc spraying  of wear-resistant  restorative  coatings  from
          cored wires (CW) of the Fe-Cr-Si-Mn-B-C alloying system was developed. A supersonic
          air jet with a Mach number of 2 was obtained at the nozzle outlet. The air jet pressure
          increased  from 0.6 to  1.2 MPa, which was accompanied by  a two-fold increase in its
          velocity (from 300 to 600 m/s), and that of molten droplets by 60–90 m/s. As a result, the
          coating hardness increased from 600 to 900 HV 0.3, abrasive wear resistance by 1.4–1.7
          times, and the level of residual tensile stresses of the first kind in the coating decreased by
          2 times.
               Based on the CW of a Fe-Cr-Si-Mn-Ti-B-C alloying system, a CW for arc spraying
          of wear-resistant coatings with an exothermic charge based on boron carbide, chromium,
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