| 摘要 |
A novel airplane comprises an airplane body (1), foldable wings (3), airscrews (2) capable of 180 degree rotation, horizontal stabilizers (6, 8) and a vertical stabilizer (7). The foldable wings (3) are connected to the airplane body via shafts, and the other part is configured as a wedge connection; the wings are provided with airstream limiting vertical plates, and the folding or unfolding of the wings is controlled by a servo motor or a stretcher bar; the front end surface of the airplane body is configured as a downward incline. The novel airplane is of low cost, is safe to fly and not subject to the usual limitations of airfield sites. |
