patent/EP-2390514-B1

http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2390514-B1

Outgoing Links

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classificationCPCInventive	http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64F5-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C65-562 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C66-721 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C66-7212 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F16B39-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F16B33-006
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filingDate	2008-08-12^^<http://www.w3.org/2001/XMLSchema#date>
grantDate	2015-12-16^^<http://www.w3.org/2001/XMLSchema#date>
inventor	http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_294062c54da22b09838112b9f8e89f54
publicationDate	2015-12-16^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber	EP-2390514-B1
titleOfInvention	Method for fastening aircraft components using a composite two-piece fastening system, and so obtained aircraft structure
priorityDate	2007-08-14^^<http://www.w3.org/2001/XMLSchema#date>
type	http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

Predicate	Subject
isDiscussedBy	http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID6556 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID128242511

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