The low cycle fatigue behaviour of titanium alloy IMI 834 was comparatively studied in bare condition and with titanium aluminide coating, at 600 °C in air, for compressor disc of aero engines. At higher values of total strain amplitudes (Δɛt/2), coated alloy has longer fatigue life as compared to the bare alloy which appears to be due to load shifting to the coat, but at lower values of Δɛt/2, coating seems to have no effect on fatigue life. Coating adheres well to the substrate and offers resistance to cyclic plastic deformation and hence is beneficial
The improvement and mechanism of the fatigue resistance of TC21 high-strength titanium alloy with a ...
The effect of surface treatment on the stress/life fatigue behavior of a titanium Ti-6Al-4V turbine ...
In the paper, on the basis of the performed tests, low-cycle fatigue characteristics (LCF) of select...
The low-cycle fatigue behaviour of titanium alloy IMI 834 was comparatively studied in bare conditio...
The low-cycle fatigue behaviour of titanium alloy IMI 834 was comparatively studied in bare conditio...
In this paper the fatigue behaviour of Ti-6Al-4V alloy coated with a TiN arc-deposited PVD film was...
Certain γ-TiAl alloys are slated for use in aeroengines where they will serve in intermediate temper...
High strength/weight ratio and effective corrosion resistance are primary reasons to use titanium al...
The primary objective of this study is to evaluate the influence of coating technique on the high cy...
This paper presents an extensive experimental study on the influence of machining parameters and coo...
Titanium alloys are used in the manufacture of gas turbine aircraft engine compressor section compon...
Aluminum alloys are widely used in the aircraft and marine industries due their good strength to wei...
High strength-to-mass ratio light alloys, such as 7075-T6 aluminium alloys and Ti-6Al-4V titanium al...
In this paper, the effect of three different thin hard coatings on the fatigue behaviour of 2011-T6 ...
The present article focuses on the influence of machining on the fatigue life of a titanium alloy: T...
The improvement and mechanism of the fatigue resistance of TC21 high-strength titanium alloy with a ...
The effect of surface treatment on the stress/life fatigue behavior of a titanium Ti-6Al-4V turbine ...
In the paper, on the basis of the performed tests, low-cycle fatigue characteristics (LCF) of select...
The low-cycle fatigue behaviour of titanium alloy IMI 834 was comparatively studied in bare conditio...
The low-cycle fatigue behaviour of titanium alloy IMI 834 was comparatively studied in bare conditio...
In this paper the fatigue behaviour of Ti-6Al-4V alloy coated with a TiN arc-deposited PVD film was...
Certain γ-TiAl alloys are slated for use in aeroengines where they will serve in intermediate temper...
High strength/weight ratio and effective corrosion resistance are primary reasons to use titanium al...
The primary objective of this study is to evaluate the influence of coating technique on the high cy...
This paper presents an extensive experimental study on the influence of machining parameters and coo...
Titanium alloys are used in the manufacture of gas turbine aircraft engine compressor section compon...
Aluminum alloys are widely used in the aircraft and marine industries due their good strength to wei...
High strength-to-mass ratio light alloys, such as 7075-T6 aluminium alloys and Ti-6Al-4V titanium al...
In this paper, the effect of three different thin hard coatings on the fatigue behaviour of 2011-T6 ...
The present article focuses on the influence of machining on the fatigue life of a titanium alloy: T...
The improvement and mechanism of the fatigue resistance of TC21 high-strength titanium alloy with a ...
The effect of surface treatment on the stress/life fatigue behavior of a titanium Ti-6Al-4V turbine ...
In the paper, on the basis of the performed tests, low-cycle fatigue characteristics (LCF) of select...