| 摘要 |
<p>The vehicle has a turbine (3) that generates air stream on an upper surface of a front wing (1) that is positioned in an inlet of a compressor. The wing (1) is constituted of the upper surface that is adjustable for providing air lift in takeoff phase, and a rigid lower surface. A rear wing (2) is positioned on an outlet of a pipe (11) and has another upper surface on which flue gas stream is applied for producing air lift force to allow takeoff and landing. The wings are arranged around the turbomachine. Injectors (7, 8) take air from the compressor.</p> |
