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PIECE DE TURBOMACHINE REVETUE D'UNE BARRIERE THERMIQUE ET PROCEDE POUR L'OBTENIR.
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.
PIECE DE TURBOMACHINE REVETUE D'UNE BARRIERE THERMIQUE ET PROCEDE POUR L'OBTENIR.
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.
PIECE DE TURBOMACHINE REVETUE D'UNE BARRIERE THERMIQUE ET PROCEDE POUR L'OBTENIR.
TURBOMACHINE PART COATED WITH A THERMAL BARRIER AND PROCESS FOR OBTAINING SAME
MIT EINER WÄRMEDÄMMUNG BESCHICHTETES TURBOMASCHINENTEIL UND VERFAHREN ZUR HERSTELLUNG DAVON
JOULIA AURÉLIEN (Autor:in) / MALIE ANDRÉ HUBERT LOUIS (Autor:in) / ANSART FLORENCE (Autor:in) / DELON ELODIE MARIE (Autor:in) / DULUARD SANDRINE (Autor:in)
24.01.2024
Patent
Elektronische Ressource
Französisch
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