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

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

Bibliographic Details
Parent link:Surface and Coatings Technology: Scientific Journal
Vol. 96, iss. 1.— 1997.— [P. 39-44]
Other Authors: Shulov V. A., Nochovnaya N. A., Ryabchikov A. I. Aleksandr Ilyich, Remnev G. E. Gennady Efimovich
Summary:Title screen
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.
Режим доступа: по договору с организацией-держателем ресурса
Language:English
Published: 1997
Subjects:
электронный ресурс
труды учёных ТПУ
ion beams
refractory alloys
service properties
Online Access:http://dx.doi.org/10.1016/S0257-8972(97)00170-9
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=645333

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