http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016078708-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-2016078708-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 according to the present invention includes a base material layer made of polycarbonate as a main material, and a covering layer provided by being laminated on one surface side of the base material layer. When the laminate 4 is burned according to the heat release test defined in ASTM E906, the maximum heat generation rate measured within 5 minutes from ignition is 65 kW / m 2 or less. It is characterized by that. [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: 63.