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PROFESSIONAL ADVICE
    developing and researching a TsMDS of this type.               below certain  values),  the  accelerating
    However, the incompleteness of the development                 mode of the UAS "breaks down" and the ion
    of this design and the urgent nature of the task at            accelerator starts operating in the plasma
    hand made us look for another technical solution.              generation  mode.  Plasma  fills  the  space
            For preliminary ion preparation and                    between the substrate and the AIS, which
    ion assistance  we used  an  autonomous gas-                   creates  conditions for  the  implementation
    discharge plasma source. The design diagram of                 of the ion-assisted mode. At a bias voltage
    the integrated plasma device included the TsMRS                of  60  V  on  the  substrate,  the  substrate
    and  the  autonomous  ion  source  (AIS),  located             surface is bombarded with low-energy ions
    coaxially in the cavity of the workpiece (Fig.2b).             that assist the process of condensation of
    An  ion source  with a  narrow  anode  layer  (UAS             the ion-plasma coating.
    of  the  "Radical"  type)  was  used  as  the  AIS.  In               This paper presents the results of the
    contrast  to  the  "Radical",  the  exit  aperture  of         development  of  individual  and  integrated
    the UAS axial magnetic system was located not                  plasma  technological devices  that  allow
    on  the  flat  end  surface  of  the  magnetic  poles,         the  application of  coatings of  various
    but  on  the  conical  surface  (Fig.  2b).  Thus,  a          architecture,  composition  and  purpose
    highly  divergent  flow  of  gas  ions  was  formed,           on  the  inner  working surfaces  of  parts  of
    which irradiated the condensation surface of the               considerable length and diameter (from 20
    coating with high-energy gas ions. At a discharge              mm and more) made of ferromagnetic and
    voltage  of  UAS  U  = 1500  V,  the  ion current  to          non-ferromagnetic structural materials.
    the treated surface was 0.25 A. it was found that
    when the gas flow rate through the UAS anode
    increases (or when the discharge voltage drops









                                                                                                         A.D. Grishkevich.
                                                            Institute of Technical Mechanics National Academy of Sciences of Ukraine
                                                                        and the State Space agencies of Ukraine, Dnepropetrovsk.










    Reference:
    1. Patent for invention No. 38845U, Ukraine, IPC С23С 14/00. Plasma device / Grishkevich A.D., applicant and patent holder Institute of Technical
    Mechanics of NASU and SSAU. - u200808700, app. 01.07.2008, publ. 26.01.2009, Bul. No. 2 - 4 p.
    2. Patent for invention No. 93471, Ukraine, IPC С23С 14/35, 14/56. Ion-plasma installation / Grishkevich A.D., Grinyuk S.I., applicant and patent
    holder Institute of Technical Mechanics of NASU and SSAU. - a201005669; declared 05/11/2010, publ. 10.02.2010, Bul. No. 23 - 4 p.
    3. Patent for invention No. 93833U, Ukraine, IPC С23С 14/00. Ion-plasma device of "hybrid" type / Grishkevich AD, applicant and patent holder
    Institute of Technical Mechanics of NASU and SSAU. –A201005613, app. 05/11/2010, publ. 03/10/2011, Bul. No. 5 - 4 p.

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