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