http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103662083-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K3-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K1-167 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K3-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K1-16 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K3-222 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01B7-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D45-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H05K3-125 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D43-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D15-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64F5-00 |
| filingDate | 2013-09-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2016-06-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2016-06-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-103662083-B |
| titleOfInvention | The method producing the airplane structural parts with the shell being provided with electrical conductive elements |
| abstract | The present invention relates to the method producing the airplane structural parts with the shell being provided with electrical conductive elements。Especially, the invention discloses the such a method for producing airplane structural parts (1), described parts have the shell (3) being provided with electrical conductive elements (17)。Said method comprising the steps of: the airplane structural parts (1) with shell (3) are provided；With predetermined pattern, the granule of conductive material (11) is applied on the outer surface (9) of shell (3) of described airplane structural parts (1) so that the granule of the conductive material gathered (11) along shell (3) outer surface (9) formed electrical conductive elements (17)；And be applied to by the granule of electrically insulating material (13) with predetermined pattern on the outer surface (9) of shell (3) of described airplane structural parts (1), so that the granule of the electrically insulating material gathered (13) forms the insulating barrier (31) of electrical conductive elements (17)。 |
| priorityDate | 2012-09-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 24.