| 摘要 |
A vertical take-off and landing aircraft (1) is disclosed. The aircraft comprises: a propulsion mechanism (2), an engine (3), a frame, seating (5), a control stick (6), and a landing undercarriage (7). The propulsion mechanism (2) includes a fan (21) to generate lift and thrust. The engine (3) provides motive power to the propulsion mechanism (2). A frame couples the propulsion mechanism (2) and the engine (3) where seating (5) is connected to and suspended from the frame so as to be swingable back and forth relative to the frame. The control stick (6) is connected to the frame and a landing undercarriage (7) is connected to the frame or the seating (5). The propulsion mechanism (2) is connected to the frame such that a drive shaft of the fan is directed vertically during landing, and the frame is moved relative to the seating (5) by manipulating the control stick (6) to change orientation of the propulsion mechanism (2). |
