| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1a34d7d2e0d09a58cb7bf4a04c81162e |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2300-611
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-31
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-12611 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1225
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1216
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1254
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C28-3215
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C28-321
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C28-325
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-288
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C30-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C28-3455
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C28-345
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1208
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1229 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-48 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C26-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C16-40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C14-10 |
| filingDate |
2008-11-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9883472ea0a8cfbc4f8f524571e0b70a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9097d87a57d6da33348216c92346af74
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_972f9d20686d856365086124cd6ac872 |
| publicationDate |
2009-06-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
CA-2645293-A1 |
| titleOfInvention |
Protective coating systems for gas turbine engine applications and methods for fabricating the same |
| abstract |
Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary method of fabricating a protective coating system on a substrate comprises forming a bond coating on the substrate, forming a silicate layer on the bond coating, forming a thermal barrier coating overlying the silicate layer, and heating the thermal barrier coating. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112759388-A |
| priorityDate |
2007-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |