Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f1001bb1c8dddcbfa07e78dc62aa6075 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5e83bc9b2cb8d1cefb764635c5c12204 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1a34d7d2e0d09a58cb7bf4a04c81162e http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_021acf37419afba225fc4a4af2e70644 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-31 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2300-611 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-12611 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1229 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/C23C18-1208 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/C23C30-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1216 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1225 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C23C18-1254 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B15-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B9-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B18-00 |
filingDate |
2011-06-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_337909f600c7b694fc927bb63c431a42 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bc58d8575c144293865f2c12d61a5220 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4a58ea3e0aa08691fa8b150106102198 |
publicationDate |
2011-12-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-2011305921-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 protective coating system comprises an aluminide-comprising bond coating disposed on a substrate, a thermal barrier coating overlying the aluminide-comprising bond coating, and a silicate layer interposed between the thermal barrier coating and the aluminide-comprising bond coating. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103206264-A |
priorityDate |
2007-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |