Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
A thermal barrier coating (208, 300) is formed over the substrate (201). A majority of the thermal barrier coating (208, 300) comprises a multi-phase material comprising a polycrystalline material including two or more phases. Each phase forms an individual grain (302, 304, 306), adjacent individual grains (302, 304, 306) are separated by grain boundaries, each phase comprises an oxide compound, the multi-phase material is formed from three or more constituents, the three or more constituents consist of different materials that are not completely soluble in each other, and the two or more phases are not completely soluble in each other and do not form only one compound.
A thermal barrier coating (208, 300) is formed over the substrate (201). A majority of the thermal barrier coating (208, 300) comprises a multi-phase material comprising a polycrystalline material including two or more phases. Each phase forms an individual grain (302, 304, 306), adjacent individual grains (302, 304, 306) are separated by grain boundaries, each phase comprises an oxide compound, the multi-phase material is formed from three or more constituents, the three or more constituents consist of different materials that are not completely soluble in each other, and the two or more phases are not completely soluble in each other and do not form only one compound.
Turbine engine components
Turbinenmotorenkomponenten
Composants de moteur à turbine
TOLPYGO VLADIMIR K (Autor:in)
06.09.2017
Patent
Elektronische Ressource
Englisch
Thermal barrier coatings for turbine engine components
Europäisches Patentamt | 2018
|Thermal barrier coatings for turbine engine components
Europäisches Patentamt | 2022
|Turbine engine components with chemical vapor infiltrated isolation layers
Europäisches Patentamt | 2019
|Probabilistic High Cycle Fatigue Analysis of Turbine Engine Components
British Library Conference Proceedings | 2000
|