发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 PROBLEM TO BE SOLVED: To minimize CO<SB>2</SB>emissions so that space flight with CO<SB>2</SB>emissions reduced to zero is fully achieved, circuit of the earth 16 times in a day is achieved, and so on, since the existing aircraft have an extremely high air resistance during flight in the atmosphere and cause extraordinary volumes of CO<SB>2</SB>emissions. SOLUTION: A metal ball gravity impact reduction turbine is driven, and a heating turbine and a cooling turbine are driven. Maximum power having the same speed and the same volume as the atmospheric pressure is set to be platinum ball power around 36,000 times the existing steam turbine. In heat production, air heated by solar light is compressed by a plurality of heat pumps and the air heated by the solar light is heated and compressed so as to recover heat. Overheated steam heat and compressed air cold are produced, dividedly preserved, and used for the rotation output for the plurality of turbines. The combined engine jet section (78B) of a solar gravity rotating airplane (39B) is driven aiming at jet propulsion by using the power around 36,000 times the existing steam turbine, speed is substantially decupled in comparison with the existing airplane, and speed for getting out of the solar system is achieved. Accordingly, the space flight with the air resistance reduced to zero is fully achieved, and a one-day trip in anywhere on the earth and space trip are fully achieved. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011169135(A) 申请公布日期 2011.09.01
申请号 JP20090282474 申请日期 2009.12.14
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA
分类号 F03G3/00 主分类号 F03G3/00
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