| 摘要 |
A vertical take-off and landing aircraft including a propulsion mechanism 2 that generates lift and thrust, a main frame 4 that supports seating 41 and a landing undercarriage 42, a subframe 5 which supports the propulsion mechanism 2 and which is arranged so as to be swingable back and forth relative to the main frame 4, motive power supply means 3 supported by the main frame 4 and supplying motive power to the propulsion mechanism 2, and a control stick 6 connected to the subframe 5, in which the propulsion mechanism 2 includes a pair of ducted fans 21L, 21R arranged on a left side and a right side, respectively, of the main frame 4, swing shafts 22 arranged in the ducted fans 21L, 21R and extending in a horizontal direction, and control vanes 23 connected to the swing shafts 22, and swinging the control vane 23 enables the subframe 5 to move relative to the main frame 4. Maneuverability can be improved with addition of control mechanisms restrained. |
