发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 PROBLEM TO BE SOLVED: To minimize the CO<SB>2</SB>emission by traveling around the Earth 16 times a day or the like through the achievement of space flight by zero CO<SB>2</SB>exhaust gas since existing aircrafts have extremely large air resistance and a huge CO<SB>2</SB>emission amount in a flight in the atmosphere. SOLUTION: In heat production, by taking metal ball liquid gravity cold turbine as core drive + various heat turbine as combined use drive, the atmospheric constant-speed, constant-volume power is set to be almost 10,000-23,000 time mercury power or the like of an existing steam turbine. Air heated by sunlight is compressed by a number of heat pumps to recover the heat of the sunlight-heated air through heating and compression thereof. Overheated steam heat production + compressed air cold production are dividedly reserve the heat to be taken as rotational output of a plurality of turbines. The cost of reaching space through theoretically best rocket jet from the vicinity of the maximum flying altitude is reduced to 1/100 or below in comparison with existing aircraft by driving a combination engine jet part (78W) solar thermal gravitational helicopter (39C) by aiming at injection propulsion to utilize the almost 23,000 time power of an existing steam turbine. A same day trip to anywhere on Earth and travel in outer space are fully achieved through the heyday of space flight by no air resistance. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011169149(A) 申请公布日期 2011.09.01
申请号 JP20090286019 申请日期 2009.12.17
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA
分类号 F01K27/02;B64C27/04;B64D27/24;F03G3/00;F03G6/00 主分类号 F01K27/02
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