| 摘要 |
FIELD: aerostation of heavier-then-air flying vehicles; manufacture of space vehicles. SUBSTANCE: method of flight through creation of pressure differential in surrounding medium between side of flying vehicle consists in creation of issue of heat on outer surface of one side of flying vehicle and escape of heat on outer surface of other side. Issue and escape of heat are created by transfer of heat through flying vehicle from one half of its outer surface to other one. Flying vehicle used for realization of this methods has outer envelope and energy source. According to first version, outer envelope made from heat-conducting material has ellipsoidal form. Ends of thermal tubes are connected to envelope inside it. Flying vehicle is provided with at least one heat pump arranged inside it. Thermal tubes are arranged in dipole groups oriented in space axes of outer envelope. These tubes are connected to at least one heat pump. According to second version, outer shell of flying vehicle is heat-conducting and electrically conducting. Connected inside this envelope are ends of conductors made form material having different electrophysical characteristics. Flying vehicle is provided with at least one energy source. EFFECT: reduced consumption of energy; increased flying speed. 4 cl, 2 dwg
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