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公开(公告)号:EP3334702A1
公开(公告)日:2018-06-20
申请号:EP17702297.7
申请日:2017-01-11
CPC分类号: C04B41/009 , C04B41/5031 , C04B41/5042 , C04B41/87 , C04B2111/00293 , C04B2111/00982 , F01D5/282 , F01D5/284 , F01D5/288 , F05D2300/6033 , C04B35/10 , C04B35/803 , C04B35/14 , C04B35/565 , C04B35/806 , C04B35/584 , C04B41/4539 , C04B41/5032
摘要: The invention relates to a coating system for turbine components, for example a gas turbine vane and/or a gas turbine blade, in particular a component which is made of a ceramic composite material "CMC" (Ceramic Matrix Component), wherein a water-tight coating is provided on the CMC, which is chemically compatible with the substrate material and/or almost pore-free.