http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-105755418-B

Outgoing Links

Predicate Object
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C4-10
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C4-134
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filingDate 2016-03-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2018-09-04-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2018-09-04-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-105755418-B
titleOfInvention A kind of ceramic fibre/whisker strengthens composite thermal barrier coating and preparation method thereof
abstract The present invention provides a kind of ceramic fibre/whisker and strengthens composite thermal barrier coating and preparation method thereof, and composite thermal barrier coating stable structure, the thermal resistance of acquisition work well, heat shock resistance and high temperature oxidation resistance are excellent.Described method includes following steps:Step 1, the composite granule of ceramic fibre/whisker and ceramic based material is prepared, mass ratio of the ceramic fibre/whisker in composite granule is 1% 95%;Step 2, the composite granule obtained using step 1 is raw material, among being distributed in the coating being prepared with making ceramic fibre/whisker even dispersion using the method for plasma spraying or laser melting coating, to obtain ceramic fibre/crystal whisker toughened composite thermal barrier coating.Fiber/whisker is distributed in the adjacent booth piece of the fused ceramic drop solidified as hardening constituent and the piece interlayer of adjacent booth piece is not associated in region in composite thermal barrier coating.It has broad application prospects in the national defence sophisticated industry such as aero-turbine and heavy duty gas turbine.
priorityDate 2016-03-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 33.