| 摘要 |
PROBLEM TO BE SOLVED: To provide various energy-conservation cycle combined engines which can reduce the discharge of CO<SB>2</SB>from aircraft by fully prospering a space flight of zero emission of CO<SB>2</SB>and by going around the earth sixteen times per day so as to solve problems that existing aircraft receive a large air resistance during the flight in the air and discharge a large amount of CO<SB>2</SB>. SOLUTION: The maximum power at the atmosphere and at the same speed and capacity of a turbine is increased to a platinum sphere power of approximately 36,000 times that of an existing steam turbine by adopting a coated-metal sphere gravity impact reduction turbine drive and a hot heat turbine+cold heat turbine drive. A sunlight-heated air is compressed by a large number of heat pumps for heating, and the heat of the sunlight-heated air is recovered. The hot heat produced by superheated steam and the cold heat produced by compressed air are stored separately to use as an output for rotating a plurality of turbines. The speed of the aircraft is increased to approximately 10 times that of a combined engine jetting part (78B), a solar heat and gravity flying ship (39G), and existing driven aircraft for jetting and propelling the aircraft using a power of approximately 36,000 times that of the existing steam turbine. The space flight with an air resistance of zero is prospered to attain a speed for escaping from the planetary system. Consequently, one-day trips and space trips can be prospered anywhere on the earth. COPYRIGHT: (C)2011,JPO&INPIT
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