In the paper there was established the influence of temperature and process time on the functional properties of aluminide layer deposited on nickel based - Inconel 713 LC superalloy. The low-activity CVD processes were done at the temperature 760 and 1050°C during 4 and 8h. The effects of aluminizing were verified by the use of optical microscope (microstructure and depth layer); scanning electron microscope and energy dispersive spectroscope (chemical composition on the surface and cross-section of aluminide layer). The high temperature oxidation resistance of superalloy was a main criterion of aluminizing process effectiveness. Therefore, the isothermal oxidation tests were performed at the temperature 1150°C during 100h in air atmospher...
Nickel superalloys are commonly used in the high temperature sections of aero- and land-based turbin...
With increasing challenges from energy and climate, it is critical to reduce the emission of greenho...
High pressure turbine blades in aircraft are subject to high temperatures, often above 1000˚C, durin...
An investigation was conducted to synthesize βNiAl coating on the nickel based superalloy Mar M247 i...
The aim of the present work was to determine the influence of chemical composition of the nickel bas...
In the paper some functional properties (hardness and oxidation resistance) of platinum and palladiu...
In the paper some functional properties (hardness and oxidation resistance) of platinum and palladiu...
The study aims to investigate the effect of Al2O3 and Al additions to Nickel-base superalloys as a c...
AbstractCyclic oxidation and hot corrosion behaviours of aluminide and Si modified aluminide diffusi...
The basic method of surface protection for aviation engine components manufactured from nickel super...
The use of thermal barrier coating systems allows superalloys to withstand higher operating temperat...
This thesis reports on investigations of high temperature oxidation resistant aluminide diffusion co...
The turbine blades in gas turbine engines need to be protected against high temperature oxidation an...
The nickel aluminides are commonly employed as a bond coat material in thermal barrier coating syste...
MCrAlY (M = Ni, Co) coatings are commonly used on gas-turbine components as oxidation resistant over...
Nickel superalloys are commonly used in the high temperature sections of aero- and land-based turbin...
With increasing challenges from energy and climate, it is critical to reduce the emission of greenho...
High pressure turbine blades in aircraft are subject to high temperatures, often above 1000˚C, durin...
An investigation was conducted to synthesize βNiAl coating on the nickel based superalloy Mar M247 i...
The aim of the present work was to determine the influence of chemical composition of the nickel bas...
In the paper some functional properties (hardness and oxidation resistance) of platinum and palladiu...
In the paper some functional properties (hardness and oxidation resistance) of platinum and palladiu...
The study aims to investigate the effect of Al2O3 and Al additions to Nickel-base superalloys as a c...
AbstractCyclic oxidation and hot corrosion behaviours of aluminide and Si modified aluminide diffusi...
The basic method of surface protection for aviation engine components manufactured from nickel super...
The use of thermal barrier coating systems allows superalloys to withstand higher operating temperat...
This thesis reports on investigations of high temperature oxidation resistant aluminide diffusion co...
The turbine blades in gas turbine engines need to be protected against high temperature oxidation an...
The nickel aluminides are commonly employed as a bond coat material in thermal barrier coating syste...
MCrAlY (M = Ni, Co) coatings are commonly used on gas-turbine components as oxidation resistant over...
Nickel superalloys are commonly used in the high temperature sections of aero- and land-based turbin...
With increasing challenges from energy and climate, it is critical to reduce the emission of greenho...
High pressure turbine blades in aircraft are subject to high temperatures, often above 1000˚C, durin...