| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_558b57c8c61df7eb6dde16dab37f4ab4
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_37f4922dfb7777b019e504b885211b8e
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b603ecd95b3b1497ae9f30752a676c0e |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-12549
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-12479
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1254
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-288
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1216
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1245 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C18-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C18-12 |
| filingDate |
2011-03-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_86f89af10924bada91af2e9469644722
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_effdfb7ed888286125b3e1f0fe7ffbc1
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9b59388d6a0edc0f3542a029e4547755
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_46ee6931f159316c5fb8f607bdf2cafa
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5465f6ed2c800f9b60f1b9771ce8cda0 |
| publicationDate |
2011-09-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
CA-2792518-A1 |
| titleOfInvention |
Method for manufacturing a thermal-barrier protection and multi-layer coating suitable for forming a thermal barrier |
| abstract |
The invention relates to a method for producing a thermal barrier protection covering a superalloy metal substrate and comprising at least one metal underlayer (13) and a yttrium-stabilized zirconia ceramic layer (14). having a columnar structure defining pores. The following steps are implemented; the impregnation of a part of the pores of the ceramic layer (14) with a zirconia-based sol is carried out by sol-gel, and in order to form an anchoring sub-layer (22), one forms on said ceramic layer surmounted by said anchoring sub-layer (22), a continuous oxide-based protective layer (20), by sol-gel, and a heat treatment is carried out, whereby an outer protective layer against CMAS attack of the thermal barrier (11). Application to the protection of aircraft engine parts. |
| priorityDate |
2010-03-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |