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 |