发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 PROBLEM TO BE SOLVED: To make CO<SB>2</SB>-emission-free space flight florescent by minimizing CO<SB>2</SB>emissions for going around the earth sixteen times a day, whereas existing airplanes have an enormous amount of CO<SB>2</SB>emission because of very great air resistance during flight in the atmosphere. SOLUTION: Coated metallic ball and mercury gravity type turbines are driven to develop mercury power having the same speed and the same capacity as the atmospheric pressure, about 23,000 times that of an existing steam turbine. A number of heat pumps are used for compressing solar-heated air to produce heat which is recovered with the solar-heated air heated and compressed. Hot superheated steam and cold compressed air are produced and dividedly conserved to serve the rotation outputs of the plurality of turbines. Thus, a solar heat gravity airship (39G) having a combined engine jet part (78W) for jet propulsion utilizing the power about 23,000 times that of the existing steam turbine is driven to reduce theoretically best cost using a jet-powered rocket for reaching space from near the maximum flight altitude of existing airplanes, down to 1/100 or smaller, thus actualizing fully popular space flight with zero air resistance and fully enjoyable one-day trip and space trip anywhere on the earth, using the rocket having a sufficient speed for breaking away from the solar system. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011185075(A) 申请公布日期 2011.09.22
申请号 JP20090297655 申请日期 2009.12.28
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA
分类号 F01K27/02;B64C35/00;B64D27/24;F03G3/00;F03G6/00 主分类号 F01K27/02
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