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filingDate 2009-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a8787b63d448a867b7311a5c70506433
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publicationDate 2011-09-22-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2011185072-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 combined best engine jet unit (78B) by solar injection propulsion solar thermal gravity helicopter (39C) drive The best aircraft from the vicinity of the maximum flight altitude of the existing aircraft The best rocket injection Space arrival cost is 1/100 or less, solar system escape velocity rocket aim, air resistance Space Flight Prime is 0, and day trips and space trips will be everywhere on earth. [Selected figure] Figure 3
priorityDate 2009-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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