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Small unmanned aerial vehicle onboard fuse mechanism assembly positioning device

A technology for assembling positioning devices and small unmanned aerial vehicles, which is used in aircraft assembly, workpiece clamping devices, manufacturing tools, etc., can solve the problems of time-consuming and labor-intensive, and cannot guarantee assembly accuracy, achieve accurate positioning, reduce debugging and adjustment costs, and improve The effect of reliability

Pending Publication Date: 2018-09-21
XIAN AISHENG TECH GRP +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to avoid the deficiencies of the prior art, the present invention provides a small UAV airborne fuze mechanism assembly and positioning device, which solves the time-consuming and labor-intensive problems of the manual assembly of the UAV warhead fuze mechanism. The problem that the assembly accuracy cannot be guaranteed saves production costs and improves labor efficiency

Method used

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  • Small unmanned aerial vehicle onboard fuse mechanism assembly positioning device
  • Small unmanned aerial vehicle onboard fuse mechanism assembly positioning device
  • Small unmanned aerial vehicle onboard fuse mechanism assembly positioning device

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Experimental program
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Embodiment Construction

[0023] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0024] Such as figure 1 , 2 As shown, a process device for the assembly and positioning of the airborne fuze mechanism in the body of a small UAV, its composition structure includes the following components: body 1, spring 2, sliding top 3, handle 4, operating rod 5, pin Axis 6.

[0025] Such as image 3 As shown, the main body 1 is the base of the device, and its shape is cylindrical, and the inside is composed of through-step holes with different functions, and functional holes are opened on the side wall. Specifically, a sliding top 3 is installed in the inner hole of its left end, and the sliding top 3 can slide left and right in the axial direction along the inner hole of the left section of the body 1, and its function of use has been completed. The right end of the sliding top 3 is equipped with an automatic return Make the sliding top 3 compress the s...

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Abstract

The invention relates to a small unmanned aerial vehicle onboard fuse mechanism assembly positioning device which comprises a body, a spring, a sliding tip, a handle, an operation rod and a pin. The body is a device base, the sliding tip is mounted in an inner hole of the left end of the body and can slide left and right along the inner hole of the body, the spring is mounted on the right end faceof the sliding tip, the right end of the spring is limited by the pin, and the handle and the operation rod are fixedly connected onto the sliding tip and used for operating the sliding tip. The device is accurate in positioning and high in production efficiency and avoids the problems of poor assembly precision and consistency caused by personal technical level difference of assemblers in the past, the assembly production efficiency of an unmanned aerial vehicle onboard fuse mechanism is improved to a certain extent, commissioning adjustment cost is directly reduced, and task executing reliability of equipment is effectively improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle assembly, in particular to a small unmanned aerial vehicle airborne fuze mechanism assembly positioning device. Background technique [0002] The assembly of the airborne fuze mechanism of small UAVs is now carried out by relying on the experience and skill level of the assemblers themselves. It is difficult to guarantee the installation standard of the mechanism and the assembly accuracy of the airborne fuze mechanism. The adjustment period is long and the efficiency is low. Consistency is poor. At the same time, because UAVs work in harsh environments such as large temperature differences, humidity, salt fog, and dust, their stability, safety, reliability, and service life directly affect the UAV's airborne fuze mechanism. Reliability and quality at work. Especially with the mass adoption of carbon fiber materials, traditional methods can no longer meet the needs of production ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B11/00B25B11/02B64F5/10
CPCB64F5/10B25B11/00B25B11/02
Inventor 王魁元马斌
Owner XIAN AISHENG TECH GRP