| 摘要 |
<p>The invention relates to a passenger and freight-carrying airplane of low or high capacity. According to the invention, the airplane comprises an aerodynamic body (A) provided, at its top part, with an aerodynamic base for mounting, sustentation and operation of the four pairs of segmented and swinging wings (19, 23, 24 and 26) placed along the entire airplane body length with the posibility of swinging under preset angles, and some pairs of swinging reaction engines (18, 25) mounted at the ends of the segmented and swinging wing pairs (19, 24) for the vertical take-off and landing, as well as other pairs of reaction engines (13, 7) provided at the bottom part, the system for swinging, from 3A to 90A , the pairs of engines (18, 25) and the pairs of segmented and swinging wings (19, 23, 24 and 26) comprises three tube-shaped concentric shafts (20, 21, 22), of which an internal resistance shaft (20) and an intermediate tube-shaped shaft (21) are provided for positioning the pairs of swinging reaction engines (18, 25), and are integral with an external tube-shaped shaft (22) for positioning the pairs of segmented and swinging wings (19, 23) which are also integral therewith.</p> |
