| 摘要 |
A composite aircraft consisting of a fixed-wing and electrically driven propellers comprises an electrically-driven-propellers power system (5) and a general controller (7). A fixed-wing power system (4) and the electrically-driven-propellers power system (5) are structurally independent of each other. The general controller (7) comprises a fixed-wing control system (71) and an electrically-driven-propellers control system (72). The general controller (7) is further used for controlling the fixed-wing control system (71) and the electrically-driven-propellers control system (72) to work separately or in a coordinated manner. The blade rotation plane of the electrically-driven-propellers power system (5 is parallel to the central axis of the aircraft body. The composite aircraft consisting of a fixed-wing and electrically driven propellers can not only take off, land and fly vertically like a helicopter, but also take off, land and fly like a fixed-wing aircraft; moreover, the two power systems can work together during taking off, landing, and flying. |
