A turbine engine part coated in at least a first ceramic layer forming a thermal barrier and including a ceramic material with first ceramic fibers dispersed in the first layer. The first layer may have a chemical composition gradient between a material for forming a thermal barrier and a material for providing protection against calcium and magnesium aluminosilicates, which is present at a greater content in an outer zone of the first layer, and/or the first layer may be porous and may present a porosity gradient such that an outer portion of the first layer presents lower porosity.
A TURBINE ENGINE PART COATED IN A THERMAL BARRIER, AND A METHOD OF OBTAINING IT
2019-08-22
Patent
Electronic Resource
English
Turbine engine part coated in a thermal barrier, and a method of obtaining it
European Patent Office | 2022
|Effect of thermal barrier coated piston crown on engine characteristics
Tema Archive | 2000
|Experimental Study of Energy Balance in Thermal Barrier Coated Diesel Engine
British Library Conference Proceedings | 2012
|Experimental Study of Energy Balance in Thermal Barrier Coated Diesel Engine
SAE Technical Papers | 2012
|