Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1ab54eb908826df87b0417f927dbfcd5 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-246 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-202 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-232 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-80 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-122 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-304 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-31 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-128 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-044 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-246 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-041 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-04 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D9-04 |
filingDate |
2017-06-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f8b9511580caf24058b53cab2a380b01 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f7f46d1a3675e26d647d38d2dd713946 |
publicationDate |
2020-06-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-2020182076-A1 |
titleOfInvention |
Static blade for a turbine diaphragm and associated turbine diaphragm |
abstract |
Static blade for an axial flow turbine comprising an aerofoil portion having a leading edge, a trailing edge, a pressure side and a suction side and radially inner and outer reinforcement portions integral with said aerofoil portion. Each reinforcement portion closely follows the shape of the section of the aerofoil portion. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112377278-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2022136397-A1 |
priorityDate |
2016-06-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |