Evaluation of feasibility of applying the technology of layer-by-layer forming by method of plasma surfacing of titanium alloy parts of components of helicopters and gas turbine engines
Saved in:
Date: | 2018 |
---|---|
Main Authors: | I. A. Petrik, S. L. Chigilejchik, T. A. Mitina, Ju. A. Marchenko, M. O. Gnatenko |
Format: | Article |
Language: | English |
Published: |
2018
|
Series: | Electrometallurgy Today |
Online Access: | http://jnas.nbuv.gov.ua/article/UJRN-0000926147 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Journal Title: | Library portal of National Academy of Sciences of Ukraine | LibNAS |
Institution
Library portal of National Academy of Sciences of Ukraine | LibNASSimilar Items
-
In-service fatigue fracture mechanisms in covered disks of a TV3-117VK helicopter turbine engine
by: Shanyavskii, A.A., et al.
Published: (2008) -
Evaluation of the possibility of manufacturing and repairing engine parts from aluminium alloys by method of additive technology
by: M. O. Gnatenko, et al.
Published: (2018) -
A STARTER-GENERATOR FOR HELICOPTERS
by: Lushchik, V. D., et al.
Published: (2013) -
Influence of pulsations of the flexible DC motor on the management process of starting the gas turbine motor helicopter
by: V. G. Bashinskij, et al.
Published: (2020) -
Electron beam welding of medium-pressure chamber of gas turbine engine
by: V. M. Nesterenkov, et al.
Published: (2015)