http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2016061699-A1

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filingDate 2014-04-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e019c27f5225634cb9afb2fe0b99950c
publicationDate 2016-03-03-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-2016061699-A1
titleOfInvention Method for analysing a fracture face of a part of a turbine engine
abstract Process for analysing a fracture or crack surface 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.
priorityDate 2013-04-22-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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