Flight device with first main rotor and second main rotor arranged below sub-rotor
A flight device that can accurately perform attitude control with a sub-rotor is provided. The flight device 10 includes an airframe 19 , an engine 30 , motors 21 , main rotors 14 , and sub-rotors 15 . The engine 30 rotates the main rotors 14 . The motors 21 rotate the sub-rotors 15 . The main rotors 14 are arranged below the sub-rotors 15 . In the flight device 10 , arranging the main rotors 14 below the sub-rotors 15 prevents the sub-rotors 15 from being affected by an air flow generated by rotation of the main rotors 14 . Accordingly, the sub-rotors 15 can provide thrusts as designed by being rotated, and the position and the attitude of the airframe 19 can be accurately adjusted.
1. A flight device comprising:
an airframe;
an engine;
a motor;
a main rotor; and
a sub-rotor, wherein
the engine rotates the main rotor,
the motor rotates the sub-rotor, and
the main rotor is arranged below the sub-rotor, the main rotor includes a first main rotor and a second main rotor,
the first main rotor is arranged at a position not overlapping the airframe, on a left side of the airframe, and
the second main rotor is arranged at a position not overlapping the airframe, on a right side of the airframe.
2. The flight device according to claim 1 , wherein the main rotor is arranged above a bottom surface of the airframe.
3. The flight device according to claim 1 , wherein a distance between a rotation center of the sub-rotor and a center of the airframe is longer than a distance between a rotation center of the main rotor and the center of the airframe.
4. The flight device according to claim 1 , wherein
the sub-rotor includes a first sub-rotor, a second sub-rotor, a third sub-rotor, and a fourth sub-rotor,
the first sub-rotor is arranged on a front-left side of the airframe,
the second sub-rotor is arranged on a rear-left side of the airframe,
the third sub-rotor is arranged on a front-right side of the airframe, and
the fourth sub-rotor is arranged on a rear-right side of the airframe.
5. The flight device according to claim 1 , wherein the main rotor and the sub-rotor are arranged at positions where the main rotor and the sub-rotor do not overlap each other.
6. A flight device comprising:
an airframe;
an engine;
a motor;
a main rotor; and
a sub-rotor, wherein
the engine rotates the main rotor,
the motor rotates the sub-rotor,
the main rotor is arranged below the sub-rotor, the main rotor includes a first main rotor and a second main rotor, and is arranged above a bottom surface of the airframe,
the first main rotor is arranged at a position not overlapping the airframe, on a left side of the airframe,
the second main rotor is arranged at a position not overlapping the airframe, on a right side of the airframe, and
a distance between a rotation center of the sub-rotor and a center of the airframe is longer than a distance between a rotation center of the main rotor and the center of the airframe.