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 heat turbine + cold turbine drive as coated metal ball gravity impact reducing turbine drive, the maximum atmospheric constant-speed, constant-volume power is set to be almost 36,000 time platinum sphere power of an existing steam turbine. Air heated by solar light 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. Solar system escape speed and almost 10 time speed in comparison with an existing aircraft are targeted by driving a combination engine jet part (78A) solar thermal gravity helicopter (39C) by aiming at injection to utilize the almost 36,000 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 JP2011169118(A) 申请公布日期 2011.09.01
申请号 JP20090279979 申请日期 2009.12.10
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA
分类号 F01K27/02;F03G3/00;F03G6/00 主分类号 F01K27/02
代理机构 代理人
主权项
地址