| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_74973199515dbabd2310245aab03e282 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-185
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-221
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-121
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-303
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-121
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-13 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-187 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D5-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-18 |
| filingDate |
2009-05-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2014-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1572652ed3385b9de44a35109670d40c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4b0249c30f82be1b899fc82c114d0710 |
| publicationDate |
2014-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
CN-102016235-B |
| titleOfInvention |
Gas turbine blade and gas turbine equipped with the same |
| abstract |
A gas turbine blade capable of increasing the heat transfer performance of a serpentine flow passage. The gas turbine blade (1), in which a plurality of cooling flow passages (12) extending from the tip end to the base end of the blade are formed in the blade from the leading edge to the trailing edge thereof, includes the serpentine flow passage formed by folding back at least two cooling flow passages (12) at the tip ends or the base ends and connecting the passages to each other. The serpentine flow passage is so formed that the cross sectional area thereof is gradually reduced from the cooling flow passage (12) on the most upstream side of the serpentine flow passage to the cooling flow passage (12) on the most downstream side thereof. |
| priorityDate |
2008-05-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |