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On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
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On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
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On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines

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On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines
Journal Article

On the Rational Choice of the Azimuthal Crystallographic Orientation of Single-Crystal Cooled Rotor Blades in Aircraft Gas Turbine Engines

2015
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Overview
The influence of the azimuthal crystallographic orientation on the strength of single-crystal cooled turbine rotor blades is studied. The effect of the cooling system features on the rational choice of the azimuthal crystallographic orientation of modern single-crystal cooled turbine rotor blades is shown. The improvement in the structure and cooling systems of single-crystal cooled turbine rotor blades makes it possible to reduce the influence of the azimuthal crystallographic orientation on their stress state.