http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20030080456-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_90b2181cd68dc34f4eca98a69cc22b53 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29K2027-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29K2063-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-3085 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C39-003 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C39-10 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C39-10 |
| filingDate | 2002-04-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f4153f9f102164e28474fb0a60d30697 |
| publicationDate | 2003-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-20030080456-A |
| titleOfInvention | Aircraft propeller manufacturing method |
| abstract | The present invention is a manufacturing method of making a propeller by combining a epoxy resin and PVC powder alumina powder in a plane propeller manufacturing method to make a high-strength synthetic epoxy resin with less shrinkage and inserting a metal plate in the center of the propeller to a mold.n n n It is a manufacturing method that increases the hardness and tensile strength by plating the propeller surface by increasing the adhesion between the epoxy resin and the metal plate by drilling a hole in the metal plate in the center of the propeller. |
| priorityDate | 2002-04-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 20.