Large drone
The invention discloses a large drone that is powered by solar energy. In addition, the drone includes a large, lightweight fuselage that not only keeps balance and stability but also reduces the required power during flight.
1. A large drone, comprising:
a fuselage comprising:
an upper layer comprising a plurality of upper support rods arranged horizontally; and
a lower layer comprising a plurality of lower support rods arranged horizontally, wherein the plurality of upper support rods correspond to the plurality of lower support rods;
a plurality of propellers respectively arranged at terminal ends of the plurality of upper support rods;
a plurality of motors corresponding to the plurality of propellers, each motor being arranged under the corresponded propeller and driving the corresponded propeller;
a solar cell module being fixed above and parallel to the upper layer to provide a power for the large drone to fly;
a flight control device controlling a flight and an attitude of the large drone;
wherein a wheelbase of the fuselage is greater than 60 cm, and the wheelbase is defined as a maximum distance between shafts of the plurality of propellers.
2. The large drone as recited in claim 1 , wherein the wheelbase is greater than 80 cm.
3. The large drone as recited in claim 1 , wherein the wheelbase is greater than 160 cm.
4. The large drone as recited in claim 1 , wherein the fuselage further comprising a plurality of longitudinal support rods between each couple of one upper support rod and one lower support rod, and two ends of each of the longitudinal support rods are respectively connected the upper support rod and the lower support rod.
5. The large drone as recited in claim 1 , wherein a distance between the upper layer and the lower layer is from 1/24 to ½ of the wheelbase.
6. The large drone as recited in claim 1 , wherein a distance between the upper layer and the lower layer is from 1/12 to ¼ of the wheelbase.
7. The large drone as recited in claim 1 , wherein the number of the upper support rods, the number of the lower support rods, the number of the propellers, and the number of the motors are four.
8. The large drone as recited in claim 1 , wherein the solar cell module comprises a plurality of solar cells, and a generated power per unit weight of each solar cell is greater than 0.25 W/g.
9. The large drone as recited in claim 1 , wherein the plurality of upper support rods and the plurality of lower support rods are made of carbon fiber.
10. The large drone as recited in claim 1 , wherein the large drone further comprises a backup battery, and the fuselage further comprises a lower support piece, and wherein one ends of the lower supporting rods are connected to the lower supporting piece, and the backup battery is disposed on the lower support sheet.
11. The large drone as recited in claim 1 , further comprising an upper support piece, wherein the flight control device is fixed to the upper support piece.
12. The large drone as recited in claim 1 , wherein a total weight of the large drone is less than or equal to 3500 g after deducting a weight of the solar cell module.