发明名称 |
METHODE DE FABRICATION D'UNE BARRIERE THERMIQUE RECOUVRANT UN SUBSTRAT METALLIQUE EN SUPERALLIAGE ET PIECE THERMOMECANIQUE RESULTANT DE CETTE METHODE DE FABRICATION |
摘要 |
<p>A fabrication method of fabricating a thermal barrier covering a superalloy metal substrate, the thermal barrier including at least an underlayer and a ceramic layer, the method including: smoothing a surface state of the underlayer by at least one physicochemical and/or mechanical process prior to depositing the ceramic layer such that a number of defects presenting a peak-to-peak difference lower than or equal to 2μm is at most five over any distance of 50μm, and then depositing the ceramic layer. The method can be applied to turbine blades.</p> |
申请公布号 |
FR2941963(B1) |
申请公布日期 |
2011.03.04 |
申请号 |
FR20090000570 |
申请日期 |
2009.02.10 |
申请人 |
SNECMA |
发明人 |
CADORET YANNICK;HERVIER SAMUEL;MONS CLAUDE;PASQUET ANNIE |
分类号 |
C23C4/02;B32B15/00;C23C14/02;F01D5/28;F01D25/00 |
主分类号 |
C23C4/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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