| 摘要 |
<p>This invention relates to a lighter-than-air saucer-shaped aircraft having a side cabin, a central cabin, a propulsion system, fixtures, strong light lamps, a control cabin and a passenger cabin. The bare weight of the aircraft is carried by the lifting force of helium in the side cabin. In the central cabin there are two helium bags for controlling flying height. The propulsion system consists of two wing engines and a tail engine. Nine nozzles of said three engines can be rotated between 0-360°. The guide vanes in the nozzles can be regulated between 0-80°. The directions of jet gases of the propulsion system are controlled by regulating the valves and by turning the rotatable nozzles and the guide vanes, so as to control flying of the aircraft. The control cabin and the passenger cabin are mounted below the loading area, the side cabin and the central cabin. The aircraft can be used for tour, amusement, passenger traffic for short distance and goods traffic for long distance.</p> |
