The paper deals with the results of research of Ti-Al-N based thin heat resistant ion-plasma coatings for titan alloy-based parts of a gas turbine engine (GTE). To carry out the research, three Ti-Al-N based fusions were taken: conglomerate, intermetallic and nitride. The analysis of oxidation process of surfaces in the range of 500° - 825°C with the use of scanning electron microscopy was performed and the key features of coatings fracture process under high-temperature oxidation conditions were identified
The main objective of this paper is to offer an ion-plasma technology for the production of Ti (tita...
The chapter describes the different aspects of ceramic materials in gas turbines. The operation cond...
Providing attractive properties like low density, high specific stiffness, high specific yield stren...
A High Power Impulse Magnetron Sputtering (HiPIMS) method for depositing TiAlN environmental barrier...
The intermetallic alloy Ti-48Al-2Cr-2Nb is used for fabrication of low pressure turbine blades, beca...
Engine designers show continued interest in γ-TiAl based titanium aluminides as light–weight structu...
The current development of new generation gamma titanium aluminides is expected to result in alloy c...
This work analyses the characteristics of functional coatings obtained by vacuum ion-plasma sputteri...
Material degradation at high temperature is a serious problem in gas turbines in aircraft. In these ...
The development of novel aero engines mainly aims on more efficient fuel consumption, decrease of th...
The thrust and efficiency of turbine engines are directly related to the operating temperature. In o...
Abstract.- Plasma spray techniques have been used to increase the Al content on existing NiCoCrAlY f...
Tutorialpg. 179-188High temperature coatings are used for protecting the high temperature turbine co...
Titanium alloys are used in the manufacture of gas turbine aircraft engine compressor section compon...
One of the major barriers limiting the suitability of TiAl intermetallic alloys for use in the deman...
The main objective of this paper is to offer an ion-plasma technology for the production of Ti (tita...
The chapter describes the different aspects of ceramic materials in gas turbines. The operation cond...
Providing attractive properties like low density, high specific stiffness, high specific yield stren...
A High Power Impulse Magnetron Sputtering (HiPIMS) method for depositing TiAlN environmental barrier...
The intermetallic alloy Ti-48Al-2Cr-2Nb is used for fabrication of low pressure turbine blades, beca...
Engine designers show continued interest in γ-TiAl based titanium aluminides as light–weight structu...
The current development of new generation gamma titanium aluminides is expected to result in alloy c...
This work analyses the characteristics of functional coatings obtained by vacuum ion-plasma sputteri...
Material degradation at high temperature is a serious problem in gas turbines in aircraft. In these ...
The development of novel aero engines mainly aims on more efficient fuel consumption, decrease of th...
The thrust and efficiency of turbine engines are directly related to the operating temperature. In o...
Abstract.- Plasma spray techniques have been used to increase the Al content on existing NiCoCrAlY f...
Tutorialpg. 179-188High temperature coatings are used for protecting the high temperature turbine co...
Titanium alloys are used in the manufacture of gas turbine aircraft engine compressor section compon...
One of the major barriers limiting the suitability of TiAl intermetallic alloys for use in the deman...
The main objective of this paper is to offer an ion-plasma technology for the production of Ti (tita...
The chapter describes the different aspects of ceramic materials in gas turbines. The operation cond...
Providing attractive properties like low density, high specific stiffness, high specific yield stren...