摘要 |
There is provided a vertical take-off and landing aircraft including: a propulsion mechanism 2 for generating lift and thrust; a power supply unit (e.g. an engine 3 as a power source) for supplying power to the propulsion mechanism 2; a main frame 4 for supporting the engine 3, a seat, and a landing undercarriage; a sub-frame 5 for supporting the propulsion mechanism 2; a frame coupling unit 6 for rotatably coupling the main frame 4 and the sub-frame 5; and a control stick 7 connected to the sub-frame 5, so that an occupant sitting on a seat 41 operates a control stick 7 thereby to move the sub-frame 5 relative to the main frame 4 so as to change the orientation of the propulsion mechanism 2. |