A fast locking mechanism for fixed-wing unmanned aerial vehicles and its application method
A fast locking, unmanned aerial vehicle technology, applied in the directions of wings, fuselage, aircraft parts, etc., can solve the problems of low flight stability, poor connection stability, time-consuming and labor-intensive, etc., and achieve reasonable structural design, convenient disassembly and assembly, and connection. Simple way to effect
Active Publication Date: 2022-03-11
湖南浩天翼航空技术有限公司
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Problems solved by technology
[0004] The purpose of the present invention is to solve the traditional disassembly method in the prior art that requires the use of tools for assembly, which is cumbersome to operate, time-consuming and laborious, and the existing quick-release structure also has complex design and poor connection stability, resulting in low flight stability. The shortcomings of the fixed-wing unmanned aerial vehicle, and a fast locking mechanism for the wing of the fixed-wing UAV and its application method
Method used
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Embodiment 1
[0034] refer to Figure 1-9 , a fast locking mechanism for the wing of a fixed-wing unmanned aerial vehicle, including a body 1 and two wings 3 that are symmetrically engaged with both sides of the body 1 , the inside of the body 1 is provided with a connecting cavity 2, and the two wings 3 Two connection blocks 4 are symmetrically fixedly connected to one side close to each other, and one side of the two connection blocks 4 extends into the connection cavity 2, and the connection cavity 2 is provided with guides for guiding and moving the two connection blocks 4 respectively. Guide assembly, two sets of first clamping components are symmetrically arranged in the connecting cavity 2, and the second clamping components are sleeved on the two sets of first clamping components, and the first clamping component and the second clamping component located in one body Both of them are engaged with the corresponding connection block 4, and the second snap-fit component brakes with th...
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The invention discloses a fast locking mechanism for a wing of a fixed-wing unmanned aerial vehicle and a method for using the same. Two connection blocks are symmetrically fixedly connected to the sides of the two wings close to each other, and one side of the two connection blocks extends into the connection cavity, and the connection cavity is provided with a guide assembly for guiding and moving the two connection blocks respectively. , there are two sets of first clamping components symmetrically arranged in the connection cavity, and the second clamping components are set on the two sets of first clamping components. The stability of the connection can also play a braking effect on each other, and the structure design is reasonable, the operation is simple, the disassembly and assembly are convenient, the clamping effect is good, the stability is strong, no tools are needed, time and effort are saved, and it has a good practicality.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a fast locking mechanism for a wing of a fixed-wing unmanned aerial vehicle and a method for using the same. Background technique [0002] Fixed-wing UAV is a type of UAV with fixed wings whose sweep angle at the outer end of the wing can be adjusted automatically or manually according to the speed. Fixed-wing UAVs have the characteristics of long battery life and relatively high arrival height. Because of their excellent functions and modular integration, they have been widely used in surveying and mapping, geology, petroleum, agriculture and forestry and other industries, and have broad market application prospects. [0003] In order to improve work efficiency and facilitate transport and portability, the existing fixed-wing drones usually design the body and wings to be detachable. However, the traditional disassembly method requires the use of tools for assem...
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IPC IPC(8): B64C1/26B64C3/00
CPCB64C1/26B64C3/00
Inventor 李昌吴东标余永光
Owner 湖南浩天翼航空技术有限公司