One of the best approaches to improving the efficiency of turbine engines is to increase their operating temperatures. A revolutionary improvement toward this goal will be the replacement of structural metallic components with silicon-based ceramic-matrix composites (CMCs). However, corrosive chemistries in combustion engines necessitate chemical protection of the structural material. Environmental Barrier Coatings (EBCs) are designed for this purpose through thermomechanical and chemical compatibility with the system. High-temperature, humid oxidation of the EBC bondcoat, a silicon layer which adheres the topcoat to the substrate, remains a critical failure mode EBC systems. This work studies the effects of chemical modifications on bon...
The internal stresses of plasma-sprayed multilayer ytterbium disilicate environmental barrier coati...
Increasing the efficiency of gas turbine engines, both for aviation and commercial power generation,...
The failure modes during steam cycling between 110 o and 1316oC of silicon-ytterbium silicate EBC sy...
The thrust and efficiency of turbine engines are directly related to the operating temperature. In o...
Recession of environmental barrier coatings (EBC) in environments containing steam is a pressing con...
Environmental Barrier Coatings (EBCs) are required for use of SiC-based composites in hot sections o...
Thermal barrier coatings (TBCs) are widely used as insulation layered at elevated temperatures in ga...
Environmental barrier coatings (EBC) are an enabling technology for the successful application of ce...
The current generation of multilayer Si/Yb2Si2O7 environmental barrier coatings (EBCs) are temperatu...
Thermal barrier coatings are applied to aeronautical and industrial gas turbine components to protec...
Silicon-based ceramic matrix composites are rapidly eroded by the high temperature water vapor that ...
Mo-Si-based alloys are being considered as high-temperature structural materials to replace Ni-based...
The ongoing development of environmental barrier coatings (EBCs) offers the prospect to implement th...
Ceramic matrix composites (CMCs) are promising materials for components in the hot section of gas tu...
Silicon carbide ceramic matrix composites (SiC/SiC-CMCs) are promising materials for application in ...
The internal stresses of plasma-sprayed multilayer ytterbium disilicate environmental barrier coati...
Increasing the efficiency of gas turbine engines, both for aviation and commercial power generation,...
The failure modes during steam cycling between 110 o and 1316oC of silicon-ytterbium silicate EBC sy...
The thrust and efficiency of turbine engines are directly related to the operating temperature. In o...
Recession of environmental barrier coatings (EBC) in environments containing steam is a pressing con...
Environmental Barrier Coatings (EBCs) are required for use of SiC-based composites in hot sections o...
Thermal barrier coatings (TBCs) are widely used as insulation layered at elevated temperatures in ga...
Environmental barrier coatings (EBC) are an enabling technology for the successful application of ce...
The current generation of multilayer Si/Yb2Si2O7 environmental barrier coatings (EBCs) are temperatu...
Thermal barrier coatings are applied to aeronautical and industrial gas turbine components to protec...
Silicon-based ceramic matrix composites are rapidly eroded by the high temperature water vapor that ...
Mo-Si-based alloys are being considered as high-temperature structural materials to replace Ni-based...
The ongoing development of environmental barrier coatings (EBCs) offers the prospect to implement th...
Ceramic matrix composites (CMCs) are promising materials for components in the hot section of gas tu...
Silicon carbide ceramic matrix composites (SiC/SiC-CMCs) are promising materials for application in ...
The internal stresses of plasma-sprayed multilayer ytterbium disilicate environmental barrier coati...
Increasing the efficiency of gas turbine engines, both for aviation and commercial power generation,...
The failure modes during steam cycling between 110 o and 1316oC of silicon-ytterbium silicate EBC sy...