发明名称 |
Manufacturing process for a refractory material, protective coating that can be obtained with this process and uses of this process and this coating |
摘要 |
This invention relates to a process for manufacturing a refractory material, a protective coating, and uses of this process and this coating. The process comprises the following steps: a) deposit on the surface of a substrate or in a mould a first dispersion containing at least one metallic compound chosen from among borides, carbides and borocarbides containing at least one transition metal, in powder form, and a resin with a coke mass content equal to at least 30% after carbonization; b) dry the resulting deposit; c) cross-link the resin; d) carbonize the resin under an inert atmosphere; e) cover the deposit with a second dispersion containing Si in powder form and a binder; f) heat the deposit to a temperature greater than or equal to the melting temperature of Si, under an inert atmosphere. Applications: manufacture of propulsion parts and fuselage and wing elements for aerospace and aeronautical applications; manufacture of heat exchangers for thermal power stations; metallurgy; chemical industry; etc.
|
申请公布号 |
US2005202282(A1) |
申请公布日期 |
2005.09.15 |
申请号 |
US20030628356 |
申请日期 |
2003.07.29 |
申请人 |
EADS SPACE TRANSPORTATION SA |
发明人 |
LESPADE PIERRE;GOURSAT PAUL;RICHET NICOLAS |
分类号 |
C04B41/89;C04B38/06;C04B41/50;C04B41/87;(IPC1-7):B32B9/00;C04B35/577 |
主分类号 |
C04B41/89 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|