发明名称 PROCEDE D'ANALYSE D'UN FACIES DE RUPTURE D'UNE PIECE DE TURBOMACHINE
摘要 <p>Process for analysing a fracture or crack surface (10) of a TiAl turbomachine part, comprising at least one of the steps consisting in: a) marking on the surface the position and the orientation of cleavage facets, so as to identify a region of fracture or crack initiation and to determine the direction of propagation of this fracture or crack, b) examining the surface and detecting the regions with the presence of equiaxed grains and/or lamellar grains, so as to evaluate the temperature at which the fracture or crack has taken place, and c) comparing the heat tintings of the surface with those of samples from a heat tinting colour chart so as to evaluate the speed of propagation of the fracture or crack.</p>
申请公布号 FR3004808(B1) 申请公布日期 2015.04.17
申请号 FR20130053660 申请日期 2013.04.22
申请人 SNECMA 发明人 COLLADON FABRICE
分类号 G01N33/20;G01N21/29;G01N21/95 主分类号 G01N33/20
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