| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c72d118f5664072de841f9c5c34b9d99 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-204
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-185
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-25
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-31
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-22
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-237
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-307
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-232 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-188 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D5-18 |
| filingDate |
2020-05-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3cbd21bcb22bf1e0ee96a2cd86fc7dd6
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ae3428be1a7e29cf263237f2200fcf8a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b7203403cf77d4c4f9d9f89c046c04f2
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_dda24cdcb3fad3cc0566549ac2db9a40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_624e55edafd0f47b7ef25a0d1c7c2f29 |
| publicationDate |
2021-01-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2021017864-A1 |
| titleOfInvention |
Tip rail cooling insert for turbine blade tip cooling system and related method |
| abstract |
A tip rail cooling insert for attaching into a tip rail pocket in a tip rail of a turbine blade is disclosed. The insert includes a first inner layer defining at least one first insert cooling channel therein, the first inner layer including a pair of spaced legs defining a first coolant collection plenum with at least the tip rail pocket for directing coolant from at least one internal cooling cavity in the turbine blade to the at least one first insert cooling channel. Each of the pair of spaced legs has an angled outer end configured to accommodate rounded inner corners of the tip rail pocket. A first outer layer is on a first side of the first inner layer, and a second outer layer is on a second side of the first inner layer. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11215074-B2 |
| priorityDate |
2018-12-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |