This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories
Prediction of the stress distribution on a 3D turbine blade coated with thermal barrier coatings (TB...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
The paper analyzes the influence of the ceramic layer on the vibration of the high pressure stage tu...
The objective of this thesis is to present the impact of the turbine blade cooling on blade material...
Advances in aircraft and land-based turbine engines have been increasing the extreme loading conditi...
The engine parts material used in gas turbines (GTs) should be resistant to high-temperature variati...
Advances in aircraft and land-based turbine engines have been increasing the extreme loading conditi...
AbstractIt is a key problem to study thermal barrier coatings (TBCs) insulation and followed stresse...
In the field of Aerospace Propulsion technology, material required to resist the maximum temperatur...
Blades of combustion turbines are extremely loaded turbojet elements, which transmit operative energ...
During rapid engine throttling operations, turbine airfoils can experience very rapid heating and co...
To study the temperature distribution and thermal-stress field in different service stages, a two-di...
Plasma-sprayed thermal barrier coatings (TBCs) will enable turbine components to operate at higher t...
ABSTRACT: Laboratory experiments were conducted to study the spallation behaviour of thermal barrier...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Prediction of the stress distribution on a 3D turbine blade coated with thermal barrier coatings (TB...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
The paper analyzes the influence of the ceramic layer on the vibration of the high pressure stage tu...
The objective of this thesis is to present the impact of the turbine blade cooling on blade material...
Advances in aircraft and land-based turbine engines have been increasing the extreme loading conditi...
The engine parts material used in gas turbines (GTs) should be resistant to high-temperature variati...
Advances in aircraft and land-based turbine engines have been increasing the extreme loading conditi...
AbstractIt is a key problem to study thermal barrier coatings (TBCs) insulation and followed stresse...
In the field of Aerospace Propulsion technology, material required to resist the maximum temperatur...
Blades of combustion turbines are extremely loaded turbojet elements, which transmit operative energ...
During rapid engine throttling operations, turbine airfoils can experience very rapid heating and co...
To study the temperature distribution and thermal-stress field in different service stages, a two-di...
Plasma-sprayed thermal barrier coatings (TBCs) will enable turbine components to operate at higher t...
ABSTRACT: Laboratory experiments were conducted to study the spallation behaviour of thermal barrier...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Prediction of the stress distribution on a 3D turbine blade coated with thermal barrier coatings (TB...
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respec...
The paper analyzes the influence of the ceramic layer on the vibration of the high pressure stage tu...