Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c426903836f4d225abf0d4c39df148e4 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29K2705-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T29-49336 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-082 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29D99-0025 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C45-1418 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D5-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29D99-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C45-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B23P15-02 |
filingDate |
2009-04-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6f8c91d78ddbd9425e6b8ce08ed7d573 |
publicationDate |
2010-04-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-2010080710-A1 |
titleOfInvention |
Stator vanes of a stator vane cascade of an aircraft gas turbine |
abstract |
A method for manufacturing a stator vane 7 of a stator vane cascade 6 of a fan structure of an aircraft gas turbine, includes circumferentially welding two essentially flat metallic sheets 10, 11. A space between the sheets 10, 11 is formed in an injection mold by a filling pressure during a plastics injection process. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8480388-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2013283820-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9217333-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9416668-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2472063-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-102536326-A |
priorityDate |
2008-04-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |