http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2016087721-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f3272933112a9429eab53ca489f5ec69 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q15-144 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q15-141 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q1-288 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q15-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q1-28 |
| filingDate | 2015-11-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cddb82a6651bf4a708635a29db218a7f |
| publicationDate | 2016-06-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | WO-2016087721-A1 |
| titleOfInvention | Method for manufacturing an antenna reflector shell, in particular of a space vehicle |
| abstract | The invention relates to a method for manufacturing an antenna reflector shell (1), wherein said shell (1) includes a sandwich structure (4), provided with a central element (5) and two skins (6, 7) arranged on either side of the central element (5) and including one skin (6) referred to as front skin, said front skin (6) reflecting electromagnetic radiation and being made of a composite material. Said method includes a perforation step that involves, during the production of the shell (1), perforating the shell (1) such as to make a plurality of holes therein that pass entirely through the shell (1). |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2021257743-A1 |
| priorityDate | 2014-12-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 18.