Modification of the properties of aircraft engine compressor blades by uninterrupted and pulsed-ion beams

V. A. Shulov, N. A. Nochovnaya, G. E. Remnev, A. I. Raybchikov

Результат исследований: Материалы для журналаСтатья

12 Цитирования (Scopus)

Аннотация

The influence of uninterrupted and arc-pulsed ion implantation, high-power ion beam treatment and final annealing regimes on the chemical composition and phase-structural state of surface layers and on the surface properties of gas turbine engine compressor blades manufactured from refractory alloys was investigated. Long-term full-scale tests of the production and irradiated compressor blades were carried out under gas turbine engine operating conditions. After completion of the tests the physical-chemical state of the blades was studied.

Язык оригиналаАнглийский
Страницы (с-по)39-44
Число страниц6
ЖурналSurface and Coatings Technology
Том96
Номер выпуска1
СостояниеОпубликовано - 3 ноя 1997

ASJC Scopus subject areas

  • Surfaces, Coatings and Films
  • Condensed Matter Physics
  • Surfaces and Interfaces

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