http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2162350-A1

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_69d44612dd4599220e6c62e678b0396b
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-31551
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-24777
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-20
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-20
filingDate 2008-06-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ce88cfe7192a731f2759abf3231e50d4
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0c0f866ba5da8953bbd85f9f3118f0d0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_090099eda73f2813d55569b8fc24513b
publicationDate 2010-03-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-2162350-A1
titleOfInvention Method of forming panels using an in-situ tape placement process and panels formed therefrom
abstract A composite panel and method of manufacture includes a support structure and a tape skin wound about the support structure. A mandrel assembly with extractable longitudinal mandrels facilitates winding of the tape skin onto the support structure. The composite panel is suitable for use in an aircraft floor system.
priorityDate 2007-06-21-04:00^^<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/substance/SID128443807
http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID5032

Total number of triples: 19.