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http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c6437cb9bd2df18ef7c02f23da18aa03
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03G3-00
filingDate 2010-01-06-04:00^^<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 2011-09-22-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2011185081-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: A metal ball mercury gravity turbine is driven, 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 with a large number of heat bombs. Solar heat heating heat compression heat recovery as heat production, superheated steam thermal production + compressed air cold heat production split storage to make the rotational output of multiple turbines, injection around 23,000 times the work rate utilization of existing steam turbine Propelled coalesced engine injection unit (78B) Solar thermal gravity helicopter (39C) driven existing aircraft The theoretical best rocket injection from the vicinity of the maximum flight altitude Targeting to the solar system escape velocity rocket with a space arrival cost of 1/100 or less, zero drag The space flight is at its peak, and day trips and space travels are everywhere on earth. [Selected figure] Figure 3
priorityDate 2010-01-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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