| 摘要 |
This invention relates to a vertical takeoff and landing aircraft with articulated wing that can be applied for operation, in particular to take off, landing on small sites and hanging still in the air. The verticaly takeoff and landing aircraft with articulated wing consists of front (1) and rear (2) wings with aerodynamic rudders (6), body (3) and prime propulsor (5), pivotally mounted in the center of the body. In the front part of the body (3) in the rear wing (2) and at the ends of the front wing (1) are mounted pivotally additional propellers (4). |
