发明名称 |
ANTIFOULING LAYER FOR COMPRESSOR BLADES |
摘要 |
The present invention relates to a composition for producing a coating having antifouling properties on a component of a turbomachine. The composition comprises a binder comprising at least one silicon-organic constituent, ceramic particles and a solvent, the ceramic particles comprising at least silicon dioxide and the silicon-organic constituent comprising at least alkoxysilane. In addition, the present invention relates to a process for producing a coating using such a composition and also a correspondingly produced coating and a component provided therewith. |
申请公布号 |
US2016009927(A1) |
申请公布日期 |
2016.01.14 |
申请号 |
US201514794036 |
申请日期 |
2015.07.08 |
申请人 |
MTU Aero Engines AG |
发明人 |
LOPEZ LAVERNIA Natividad;NIEGL Max;HEUSING Melanie |
分类号 |
C09D5/16;F01D5/28;C08K3/36;C09D183/06;C08K3/22 |
主分类号 |
C09D5/16 |
代理机构 |
|
代理人 |
|
主权项 |
1. A composition for producing a coating having antifouling properties for a component of a turbomachine, wherein the composition comprises a binder comprising at least one silicon-organic constituent that comprises at least one alkoxysilane, ceramic particles which comprise at least silicon dioxide, and a solvent. |
地址 |
Munich DE |