http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2006144780-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_18573e4267a393c689d9f7c9c64055d7 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c6437cb9bd2df18ef7c02f23da18aa03 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01K7-16 |
| filingDate | 2005-08-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a8787b63d448a867b7311a5c70506433 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4a63648a6cd09ce929f1b8cd8021103e |
| publicationDate | 2006-06-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2006144780-A |
| titleOfInvention | Various energy conservation cycle coalescence engine |
| abstract | [PROBLEMS] The existing rocket is an improvement of the outdated invention when it is enough to generate a recoil, injecting high temperature combustion gas of 1/1517 weight of water and bringing the recoil closer to 1/1517 of water is a large loss. As an energy storage cycle combined engine, water is mounted in a combustion part and an outer peripheral container, and a stopper is provided at a nozzle nozzle part to ignite and burn, and the stopper is fired when rising to an optimum pressure. Composed of heavy metal, etc. to increase the recoil, mercury etc. is mixed in the water in the combustion part bag and injected in order of heaviest, so that mercury and plugs can be recovered, and the maximum recoil is burned at high temperature 1517 * 13.5 = 21208.5 times that of the gas, and the inside of the outer container is also burned as an explosion pressure of the combustion gas, water repellent action, high temperature vaporization film, magnet repulsion, etc. After the injection of the bag and the combustion gas injection, the high temperature water in the outer container is sucked and accelerated by the combustion gas explosion speed and the principle of spraying, and the recoil is increased 10 to 100 times that of the same fuel existing rocket. [Selection] Figure 41 |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-100425819-C |
| priorityDate | 2004-10-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 40.