http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016533934-A
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-1492 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D15-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C03C10-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B17-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C03C27-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D15-12 |
| filingDate | 2014-04-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2016-11-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2016533934-A |
| titleOfInvention | Glass panels for spacecraft |
| abstract | The present invention relates to a glass panel for aircraft suitable for semi-orbital flight and air flight, the glass panel comprising an outer panel (1) made of polycarbonate or aluminosilicate for heat resistance. The main panel (2) for pressure resistance, which is sized according to the standard airplane safety factor, and with the minimum pressure limit, providing redundancy for the main panel It has an inner panel (3), the outer panel, the main panel and the inner redundant panel are separated from each other by a space (5, 6). The invention also relates to an aircraft having a windshield element and a machine window made using the glass panel. [Selection] Figure 1 |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016179774-A |
| priorityDate | 2013-04-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 28.