Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 39-44 |
| Number of pages | 6 |
| Journal | Surface and Coatings Technology |
| Volume | 96 |
| Issue number | 1 |
| Publication status | Published - 3 Nov 1997 |
Keywords
- Ion beam
- Refractory alloys
- Service properties
ASJC Scopus subject areas
- Surfaces, Coatings and Films
- Condensed Matter Physics
- Surfaces and Interfaces
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Shulov, V. A., Nochovnaya, N. A., Remnev, G. E., & Raybchikov, A. I. (1997). Modification of the properties of aircraft engine compressor blades by uninterrupted and pulsed-ion beams. Surface and Coatings Technology, 96(1), 39-44.