Electrolytic-plasma method of removing the heat-resistant coating from the surface of nickel alloy products

Pavlova T.V., Dobrynin D.A., Avanesyan T.G., Muboyadzhyan S.A.
Pavlova T.V., Dobrynin D.A., Avanesyan T.G., Muboyadzhyan S.A. Electrolytic-plasma method of removing the heat-resistant coating from the surface of nickel alloy products // Proceedings of VIAM. 2018. No. 5. DOI: 10.18577/2307-6046-2018-0-5-90-100. URL: https://test.viam.ru/en/journal/2018/5/10
Keywords
electrolyte-plasma treatment, coating removal, nickel alloy, microdischarge, gas turbine engine, fluorine ion.
Abstract

To increase the reliability and the service life of gas turbine engine (GTE) blades, heat-resistant coatings are used. The repeated use of the GTE blades after their operation or in violation of the technology of applying protective coatings is possible only in case of removing the defective coating and subsequent preparation of the blade surface for its repeated application. The currently used surface preparation methods for re-applying protective coatings are based on the preliminary cleaning of the GTE blades from the combustion products of the fuel, removal of protective coatings and surface finishing. A comparative analysis of traditional methods of removing spent coatings has shown that the electrolytic-plasma treatment method is distinguished by high productivity, high quality of the treated surface, no need for intermediate preparation stages, and its environmental friendliness. The disadvantages of this method include the inability to process the internal cavities of parts, a

Reference list
  1. Kablov E.N., Ospennikova O.G., Petrushin N.V., Visik E.M. Monokristallicheskij zharoprochnyj nikelevyj splav novogo pokoleniya s nizkoj plotnostyu [Single-crystal nickel-based superalloy of a new generation with low-density] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 14–25. DOI: 10.18577/2071-9140-2015-0-2-14-25.
  2. Kablov E.N. Strategicheskie napravleniya razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period to 2030] // Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
  3. Kablov E.N., Muboyadzhyan S.A. Zharostojkie i teplozashhitnye pokrytiya dlya lopatok turbiny vysokogo davleniya perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTE] // Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
  4. Kablov E.N., Startsev O.V., Medvedev I.M. Obzor zarubezhnogo opyta issledovanij korrozii i sredstv zashhity ot korrozii [Review of international experience on corrosion and corrosion protection] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 76–87. DOI: 10.18577/2071-9140-2015-0-2-76-87.
  5. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Pomelov YA.A. Ionno-plazmennye zashchitnye pokrytiya dlya lopatok gazoturbinnykh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] // Konversiya v mashinostroenii. 1999. №2. S.42–47.
  6. Muboyadzhyan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnyayushhie ionno-plazmennye pokrytiya dlya lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTE compressor] // Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.
  7. Kablov D.E., Belyaev M.S., Sidorov V.V., Min P.G. Vliyanie primesej sery i fosfora na malociklovuyu ustalost monokristallov zharoprochnogo splava ZhS36-VI [The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 25–28. DOI: 10.18577/2071-9140-2015-0-4-25-28.
  8. Kablov D.E., Sidorov V.V., Budinovskij S.A., Min P.G. Vliyanie primesi sery na zharostojkost monokristallov zharoprochnogo splava ZhS36-VI s zashhitnym pokrytiem [The influence of sulfur impurity on heat resistance of single crystals of ZhS36-VI alloy with protective coating] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 20–23. DOI: 10.18577/2071-9140-2016-0-1-20-23.
  9. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., YAgodkin YU.D. Perspektivy primeneniya ionno-plazmennoj tekhnologii vysokikh energij dlya mezhresursnogo remonta lopatok turbin [Perspectives of application of ion-plasma technology of high energy for interresource repair of blades of turbines] // Aviacionnye materialy i tehnologii. 2002. №1. S. 6–13.
  10. Method for cleaning metal parts with elemental fluorine: pat. US4188237A; publ. 02.02.78.
  11. Method of removing a thermal barrier coating: pat. US6238743B1; publ. 20.01.00.
  12. Shoe form: pat. US1784661A; publ. 24.10.29.
  13. Sposob remonta lopatok turbiny gazoturbinnogo dvigatelya: pat. 2367554 Ros. Federatsiya [Way of repair of turbine blades of the gas turbine engine: pat. 2367554 Rus. Federation]; opubl. 08.08.07.
  14. Rastvor dlya udaleniya alyuminijsoderzhashchikh mnogokomponentnykh zharostojkikh pokrytij s nikelevykh splavov: pat. 1324344 Ros. Federatsiya [Solution for removal of aluminum containing multicomponent heat resisting coverings from nickel alloys: pat. 1324344 Rus. Federation]; opubl. 07.09.85.
  15. Sposob udaleniya pokrytiya s metallicheskoj podlozhki: pat. 2094546 Ros. Federatsiya [Way of removal of covering from metal substrate: pat. 2094546 Rus. Federation]; opubl. 04.03.95.
  16. Process for removing chromide coatings from metal substrates, and related compositions: pat. US6953533B2; publ. 16.06.03.
  17. Method for removing aluminide coating from metal substrate and turbine engine part so treated: pat. US7008553B2; publ. 09.01. 03.
  18. Method for chemically stripping a cobalt-base substrate: pat. US5944909A; publ. 02.02.98
  19. Process of selectively removing layers of a thermal barrier coating system: pat. US6955308B2; publ. 23.06.03.
  20. Method of removing a coating from a substrate: pat. US6905396B1; publ. 20.11.03.
  21. Chemical stripping composition and method: pat. US8859479B2; publ. 26.09.11.
  22. Method of decoating a turbine blade: United States paten US6660102B2; publ. 27.12.00.
  23. Process for applying a protective layer: pat. US7736704B2; publ. 15.09.04.
  24. Method for removal of surface layers of metallic coatings: pat. US6036995A; publ. 31.01.97.
  25. Kulikov I.S., Vashchenko S.V., Kamenev A.YA. Elektrolitno-plazmennaya obrabotka materialov [Electrolit plasma processing of materials]. Minsk: Belоruskaya nauka, 2010. 232 s.