Flight vehicle
A flight vehicle includes a rotor shaft projecting upward from a body; a rotor head connected to the rotor shaft; and a pair of plate structures located at the upper side of the body and extending in a front-rear direction at right and left sides of the rotor shaft. Each of the pair of plate structures includes a front end, a rear end, an inner surface facing inward in a left-right direction, and an outer surface facing outward in the left-right direction. The front ends of the pair of plate structures are located away from each other in the left-right direction. The rear ends of the pair of plate structures are located away from each other in the left-right direction. During forward flight, pressure at a side where the outer surface is located becomes lower than pressure at a side where the inner surface is located.
1. A flight vehicle comprising:
a body;
a rotor shaft projecting upward from the body;
a rotor head connected to the rotor shaft at an upper side of the body; and
a pair of plate structures located at the upper side of the body and extending in a front-rear direction at right and left sides of the rotor shaft, wherein:
each of the pair of plate structures includes a front end, a rear end, an inner surface facing inward in a left-right direction, and an outer surface facing outward in the left-right direction;
the front ends of the pair of plate structures are located away from each other in the left-right direction;
the rear ends of the pair of plate structures are located away from each other in the left-right direction; and
each of the pair of plate structures has such a shape that during forward flight, pressure at a side where the outer surface is located becomes lower than pressure at a side where the inner surface is located, thereby generating a vertical vortex that flows upward from a region between the pair of plate structures and through a wake region of the rotor head to suppress a pressure decrease in the wake region.
2. The flight vehicle according to claim 1 , wherein each of the inner surfaces of the pair of plate structures diagonally extends toward an inside in the left-right direction and a rear side to increase airflow velocity along the outer surface during forward flight.
3. The flight vehicle according to claim 1 , wherein each of the outer surfaces of the pair of plate structures diagonally extends toward an inside in the left-right direction and a rear side.
4. The flight vehicle according to claim 1 , wherein each of the pair of plate structures has an arch shape projecting outward in the left-right direction.
5. The flight vehicle according to claim 1 , wherein the rear ends of the pair of plate structures are located in front of a rear end of a rotation trajectory of a radially outer end of the rotor head.
6. The flight vehicle according to claim 1 , wherein a distance between the rear ends of the pair of plate structures in the left-right direction is a value that is twice or more a maximum height of the plate structure.
7. The flight vehicle according to claim 1 , wherein a distance between the rear ends of the pair of plate structures in the left-right direction is a value that is six times or less a maximum height of the plate structure, such that the vertical vortex generated by each of the pair of plate structures reaches the wake region of the rotor head without interference between the vertical vortices.
8. The flight vehicle according to claim 1 , wherein:
the body includes a top portion that defines an upper opening through which the rotor shaft extends; and
the top portion includes a rear portion located behind the rear ends of the plate structures, the rear portion tapering toward a rear side to promote upward flow of the vertical vortices.
9. The flight vehicle according to claim 1 , wherein front ends of the plate structures are located in front of the rotor shaft, and
rear ends of the plate structures are located behind of the rotor shaft.
10. The flight vehicle according to claim 9 , wherein a first distance between the front ends of the pair of plate structures in a left-right direction is longer than a second distance between the rear ends of the pair of plate structures in the left-right direction.
11. The flight vehicle according to claim 1 , wherein the upper side of the body tapers in the front-rear direction.
12. The flight vehicle according to claim 7 , wherein front ends of the plate structures are located in front of the rotor shaft, and
rear ends of the plate structures are located behind of the rotor shaft.
13. The flight vehicle according to claim 12 , wherein a first distance between the front ends of the pair of plate structures in a left-right direction is longer than a second distance between the rear ends of the pair of plate structures in the left-right direction.
14. The flight vehicle according to claim 13 , wherein the upper side of the body tapers in the front-rear direction.