Six-rotor quick-release unmanned aerial vehicle arm

Abstract

The invention provides a six-rotor quick-release unmanned aerial vehicle arm. The six-rotor quick-release unmanned aerial vehicle arm comprises a blade, a brushless motor, an electronic speed-regulating module, a blade arm carbon tube, a locking block, an arm fixing shell, an arm metal frame, a fixing buckle, a spring and a male head, wherein the electronic speed-regulating module is connected with the tail of the blade arm carbon tube; the brushless motor is located above the electronic speed-regulating module; the blade is fixed to the upper portion of the brushless motor; the locking block is inserted into the top of the blade arm carbon tube; the arm fixing shell is arranged outside the top of the blade arm carbon tube in a sleeving mode; and the fixing buckle is fixed to the inner side of the arm fixing shell. The six-rotor quick-release unmanned aerial vehicle arm has a high degree of integration and high utilization rate, all the parts can be replaced, disassembling and maintenance are convenient, cost is low, and the arm can be manufactured with high efficiency; and when the six-rotor quick-release unmanned aerial vehicle arm is in use, self-locking can be achieved, and disassembling is convenient.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicles, and in particular relates to a quick-release arm of a six-rotor unmanned aerial vehicle. Background technique [0002] Today, with the rapid development of drones, the corresponding drone arms are various, and the structures of all kinds of arms are similar, and the common arms on the market are simple carbon tube fixing or simple folding mechanisms. Among them, the assembly is inconvenient, it is not easy to carry, and it is difficult to replace. At the same time, the integration of each arm is not high, and the electronic speed control modules are bundled in various ways, which makes the center of gravity of the aircraft arm inconsistent, and the overall center of gravity is prone to sideways deviation, which virtually increases the power of the aircraft. Energy consumption increases aircraft safety hazards and reduces aircraft flight time and service life. Prolonged use will cause the ...

AI Technical Summary

Problems solved by technology

[0002] Today, with the rapid development of drones, the corresponding drone arms are various, and the structures of all kinds of arms are similar, and the common arms on the market are simple carbon tube fixing or simple folding mechanisms. Among them, the assembly is inconvenient, it is not easy to carry, and it is difficult to replace. At the same time, the integration of each arm is not high, and the electronic speed control modules are bundled in various ways, which makes the center of gravity of the aircraft arm inconsistent, and the overall center of gravity is prone to sideways deviation, which virtually increases the power of the aircraft. Energy consumption, increasing aircraft safety hazards, reducing aircraft flight time and service life

Prolonged use will cause physical fatigue of the operator, haggard heart, and reduce work efficiency

At the same time, in the process of component manufacturing, precious assembly and manufacturing time is wasted, which increases manufacturing costs virtually, and cannot achieve efficient small-batch customization

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