UNMANNED AERIAL VEHICLE
First Claim
1. An unmanned aerial vehicle, comprising:
- a fuselage having a battery accommodation cavity;
a plurality of arms, wherein each arm is coupled to the fuselage;
a propulsion assembly mounted on the each arm, wherein the propulsion assembly comprises a propeller and a motor, the motor being configured to rotate the propeller in order to generate lift force;
at least two battery blocks, wherein the at least two battery blocks are mounted inside the battery accommodation cavity; and
an electronic board disposed inside the fuselage, wherein the electronic board comprise at least one of a flight control board, an electronic speed control board, a steering driving board and a radar electronic board;
wherein the at least two battery blocks power the electronic board at the same time.
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Accused Products
Abstract
The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.
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Citations
19 Claims
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1. An unmanned aerial vehicle, comprising:
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a fuselage having a battery accommodation cavity; a plurality of arms, wherein each arm is coupled to the fuselage; a propulsion assembly mounted on the each arm, wherein the propulsion assembly comprises a propeller and a motor, the motor being configured to rotate the propeller in order to generate lift force; at least two battery blocks, wherein the at least two battery blocks are mounted inside the battery accommodation cavity; and an electronic board disposed inside the fuselage, wherein the electronic board comprise at least one of a flight control board, an electronic speed control board, a steering driving board and a radar electronic board; wherein the at least two battery blocks power the electronic board at the same time. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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Specification