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Kinetics and Mechanisms of Degradation of the Surface Layers of Gas-Turbine Engine Structural Components Under Cyclic Thermal Loading During Initiation and Propagation of Thermal Fatigue Cracks

by Buiskikh, K. P. , Feofentov, N. N. , Kravchuk, L. V. , Kiselevskaya, S. G. , Zadvornyi, E. A.

in Characterization and Evaluation of Materials / Chemistry and Materials Science / Classical Mechanics / Composite materials / Corrosion / Crack initiation / Crack propagation / Degradation / Fatigue / Fatigue cracks / Fatigue failure / Fatigue testing machines / Fracture mechanics / Gas turbine engines / Gas-turbines / Heat resisting alloys / High temperature / Investigations / Materials / Materials Science / Metal fatigue / Mouth / Oxidation / Propagation / Solid Mechanics / Surface layers / Temperature / Thermal cycling / Thermal fatigue

2016

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Kinetics and Mechanisms of Degradation of the Surface Layers of Gas-Turbine Engine Structural Components Under Cyclic Thermal Loading During Initiation and Propagation of Thermal Fatigue Cracks

by Buiskikh, K. P. , Feofentov, N. N. , Kravchuk, L. V. , Kiselevskaya, S. G. , Zadvornyi, E. A.

2016

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Kinetics and Mechanisms of Degradation of the Surface Layers of Gas-Turbine Engine Structural Components Under Cyclic Thermal Loading During Initiation and Propagation of Thermal Fatigue Cracks

by Buiskikh, K. P. , Feofentov, N. N. , Kravchuk, L. V. , Kiselevskaya, S. G. , Zadvornyi, E. A.

2016

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Journal Article

Kinetics and Mechanisms of Degradation of the Surface Layers of Gas-Turbine Engine Structural Components Under Cyclic Thermal Loading During Initiation and Propagation of Thermal Fatigue Cracks

Buiskikh, K. P.,

Feofentov, N. N.,

Kravchuk, L. V.,

Kiselevskaya, S. G.,

Zadvornyi, E. A.

2016

Overview

Studies of surface layer material degradation of the most loaded elements of gas turbine engine structural components revealed the essential changes in the structure and elemental composition of this layer in the thermal fatigue crack initiation zones, as well as along the propagating crack lips. The intensity of the observed changes implies the necessity of their account in the stress-strain state calculations and residual life estimations of high-temperature structural components of gas turbine engines.

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Publisher

Springer US,Springer,Springer Nature B.V

Subject

Characterization and Evaluation of Materials

/ Chemistry and Materials Science

/ Classical Mechanics

/ Composite materials

/ Corrosion

/ Crack initiation

/ Crack propagation