http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016078707-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b19eaa8e535da4e4bceed99917a68153 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D11-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B27-36 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-00 |
| filingDate | 2014-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_898deaeb0ab1cc5bc1c6de30446191f2 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_918a84189f4e7b0880d260eeaf29781a |
| publicationDate | 2016-05-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2016078707-A |
| titleOfInvention | Aircraft interior materials and aircraft |
| abstract | An aircraft interior material that is reduced in weight and has excellent flame retardancy while securing excellent strength, and an aircraft having excellent reliability including the aircraft interior material. An aircraft interior material 1 of the present invention is provided with a base material layer 2 made of polycarbonate as a main material and laminated on one surface side of the base material layer 2, and is made up of polycarbonate as a main material. And a laminate 4 including the coating layer 3 containing at least one element selected from the group consisting of phosphorus, bromine and silicon. [Selection] Figure 1 |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11370144-B2 |
| priorityDate | 2014-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 69.