http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2011185075-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c6437cb9bd2df18ef7c02f23da18aa03 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_18573e4267a393c689d9f7c9c64055d7 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02E10-46 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C35-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03G3-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03G6-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01K27-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-24 |
| filingDate | 2009-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4a63648a6cd09ce929f1b8cd8021103e http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a8787b63d448a867b7311a5c70506433 |
| publicationDate | 2011-09-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2011185075-A |
| titleOfInvention | Various energy conservation cycle union engine |
| abstract | An object of the present invention is to reduce the amount of CO2 emissions, such as making 16 orbits of the earth in a day as a space flight burst of CO2 exhaust 0, with a large amount of air resistance and a huge amount of CO2 emissions when flying in the atmosphere. SOLUTION: The coated metal sphere mercury gravity turbine is driven, and the atmospheric pressure same speed same volume work rate is about 23,000 times mercury work rate etc. of the existing steam turbine, and the solar heating air is compressed by a large number of heat bombs. Then, as heat production to recover the heat and compression heat of solar heating air, superheated steam thermal production + compressed air cold heat production divided storage to make the rotational output of multiple turbines, use of 23,000 times power factor of existing steam turbine The combination of the engine jet part (78W) by solar propulsion and the propulsion of the thermal gravitation flight vessel (39G) driven by the existing aircraft The theoretical best rocket from near the top flight altitude The rocket arrival space rocket cost is 1/100 or less, solar system escape velocity rocket aim, air With a resistance to zero flight, we will make day trips and space trips everywhere on earth. [Selected figure] Figure 3 |
| priorityDate | 2009-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 29.