http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RO-126729-A2
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a22dc556beb64b6b47d8a3c00369df4e |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H02N3-00 |
| filingDate | 2006-09-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_457b884a670fc58da17b9c8fa854abee |
| publicationDate | 2011-09-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | RO-126729-A2 |
| titleOfInvention | IONIC PROPULSER |
| abstract | The invention relates to an ionic propellant for use in the propulsion of land, air, water and space vehicles. The ionic propellant according to the invention is an ion-generating and accelerating system and consists of energy sources (1), control systems (2), ion generator (3), ionisation turbine type, ion accelerator 4), a resistance structure (5) and an outlet nozzle / nozzle (6), the propulsion being carried out by means of a propulsion fluid (7) running from the fuel tanks (7a) through some pipes (7b, 7c) , in molecular, liquid or gaseous form, enters the ionisation turbine (3) and exits as ions (8) which are accelerated in the accelerator (4) by acceleration cells (4a), then discharged through the nozzle / evacuation nozzles (6), propelling the vehicle. |
| priorityDate | 2006-09-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 32.