A welding positioning device for the engine pipe support of a drone

By designing the welding positioning device of the pipe body bracket of the UAV engine, and using bolts and nuts to position and tighten the pipe body, the problems of dimensional deviation and low assembly reliability during welding positioning are solved, and the accuracy control and reliable assembly of the engine bracket are achieved.

CN116551285BActive Publication Date: 2025-06-24BEIJING NORTH VEHICLE GROUP CORP

Patent Information

Application Number
CN202310542377.9
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-05-15
Publication Date
2025-06-24
Estimated Expiration
2043-05-15

AI Technical Summary

Technical Problem

The prior art has problems of dimensional deviation and low assembly reliability in the welding positioning process of the pipe body bracket of the drone engine.

Method used

A welded positioning device for pipe body brackets of the drone engine is designed, including a first positioning bracket, a second positioning bracket and a third positioning bracket. The pipe body is positioned and tightened by bolts and nuts to ensure the precise combination between each pipe body.

Benefits of technology

The accuracy control and size requirements of the engine bracket are realized, ensuring reliable assembly and stable operation of the engine, and providing reliable power support for the drone.

✦ Generated by Eureka AI based on patent content.

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    Figure CN116551285B_ABST
Patent Text Reader

Abstract

The present invention provides a welding positioning device for an engine pipe body bracket of a drone, which includes a first positioning bracket, a second positioning bracket and a third positioning bracket, and is respectively used for accurately positioning the first pipe body, the second pipe body and the third pipe body of the engine pipe body bracket. Each pipe body penetrates into a pin column with holes to form an assembly base point of the engine. Bolts and nuts are used to penetrate into the pipe body pin column holes to position and fasten the pipe bodies, which can ensure the positioning accuracy of the engine assembly base point and the reliability of the positioning method. According to the correlation between the pipe bodies of the drone bracket, the engine bracket welding positioning device can combine the pipe bodies to form an accurate positioning of the bracket. By accurately positioning the engine bracket, the present invention enables the engine bracket to meet the accuracy requirements specified in the design drawings, meet the installation conditions for the assembly of the drone engine, ensure the stability of the engine function, and provide reliable power support for the drone.
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Description

Technical Field

[0001] The invention belongs to the technical field of positioning welding, and particularly relates to a welding positioning device for an engine pipe bracket of an unmanned aerial vehicle (UAV). Background Art

[0002] The engine of a certain type of UAV (airframe) is installed in a pipe bracket composed of multiple pipe bodies. The pipe bracket is combined by welding to meet certain spatial position requirements and achieve the dimensional accuracy of welding. The original operation method is to use measuring tools such as a square and a tape measure to lap and combine the three pipe bodies that make up the pipe bracket with the relevant pipe bodies respectively according to the drawing requirements to construct the pipe structure framework of the engine. Due to certain errors in manual measurement and the bending process of the pipe bodies themselves, dimensional deviations will also occur, resulting in large dimensional deviations after welding, which cannot meet the engine installation requirements of the UAV and reduce the reliability of engine assembly. Summary of the Invention

[0003] (1) Technical Problems to be Solved

[0004] The invention provides a welding positioning device for an engine pipe bracket of an unmanned aerial vehicle to solve the welding positioning requirements between the pipe bodies in the pipe bracket, achieve the welding positioning accuracy of the pipe bracket, enable the effective assembly of the UAV engine, and realize the technical problem of reliable operation of the engine.

[0005] (2) Technical Solutions

[0006] To solve the above technical problems, the invention provides a welding positioning device for an engine pipe bracket of an unmanned aerial vehicle. The welding positioning device includes a first positioning bracket, a second positioning bracket, and a third positioning bracket, which are respectively used to accurately position the first pipe body, the second pipe body, and the third pipe body of the engine pipe bracket. Among them, the first positioning bracket is located at the front of the entire positioning device and is used to position the first pipe body of the engine bracket. The second positioning bracket is located at the upper rear side of the first positioning bracket and is used to position the second pipe body of the engine bracket. The third positioning bracket is located at the lower rear side of the first positioning bracket, and the second positioning bracket is above the third positioning bracket and is used to position the third pipe body of the engine bracket. The entire positioning device forms mutual positioning accuracy requirements between the pipe bodies through the positioning and fastening of the first pipe body, the second pipe body, and the third pipe body, achieving the accuracy control and dimensional requirements of the engine bracket.

[0007] Further, the first positioning bracket includes a first cross beam and first longitudinal beams. Two first longitudinal beams are fixedly connected to both ends of the first cross beam. The rear ends of the first longitudinal beams are fixedly connected to the support rods of the third positioning bracket. A positioning attachment base is installed at the front end of each first longitudinal beam. A bolt and a nut are provided on each positioning attachment base. When positioning, the bolt penetrates through the positioning attachment base and the pin hole of the first pipe body, and after connecting the first longitudinal beam with the first pipe body, it is tightened and fixed with a nut; the second positioning bracket includes a second cross beam, and the second cross beam is fixedly connected to the tops of the two support rods of the third positioning bracket. Positioning attachment bases are installed at both ends of the second cross beam. A bolt and a nut are provided on each positioning attachment base. When positioning, the bolt penetrates through the positioning attachment base and the pin hole of the second pipe, and after connecting the second cross beam with the second pipe body, it is tightened and fixed with a nut; the third positioning bracket includes a third cross beam and support rods, and the third cross beam is fixedly connected to the bottoms of the two support rods. Positioning attachment bases are installed at both ends of the third cross beam. A bolt and a nut are provided on each positioning attachment base. When positioning, the bolt penetrates through the positioning attachment base and the pin hole of the third pipe body, and after connecting the third cross beam with the third pipe body, it is tightened and fixed with a nut.

[0008] Further, a reinforcing rib is connected between the first longitudinal beam and the support rod.

[0009] Further, the first cross beam and the first longitudinal beams are connected by welding.

[0010] Further, the third cross beam and the support rods are connected by welding.

[0011] Further, the positioning attachment base is welded to the front end of the first longitudinal beam.

[0012] Further, the positioning attachment bases are welded to both ends of the second cross beam.

[0013] Further, the positioning attachment bases are welded to both ends of the third cross beam.

[0014] (III) Beneficial Effects

[0015] The present invention provides a welding positioning device for an unmanned aerial vehicle engine pipe bracket, including a first positioning bracket, a second positioning bracket and a third positioning bracket, which are respectively used to accurately position the first pipe body, the second pipe body and the third pipe body of the engine pipe bracket. Each pipe body penetrates through a pin column with holes to form an assembly base point of the engine. Bolts and nuts are used to penetrate through the pin holes of the pipe bodies to position and fasten the pipe bodies, which can ensure the positioning accuracy of the engine assembly base point and the reliability of the positioning method. According to the correlation between the pipe bodies of the unmanned aerial vehicle bracket, the engine bracket welding positioning device can combine each pipe body to form an accurate positioning of the bracket. Through the accurate positioning of the engine bracket, the engine bracket meets the accuracy requirements specified in the design drawings, meets the installation conditions for the assembly of the unmanned aerial vehicle engine, ensures the stability of the engine function, and provides a reliable power support for the unmanned aerial vehicle. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 is the front view of the welding positioning device for the pipe support of the present invention;

[0017] Figure 2 is the top view of the welding positioning device for the pipe support of the present invention.

[0018] Figure 3 is the schematic diagram of the working principle of the welding positioning device for the pipe support of the present invention;

[0019] Figure 4 is the schematic diagram of the structure of the first positioning bracket in the present invention;

[0020] Figure 5 is the schematic diagram of the structure of the second positioning bracket in the present invention;

[0021] Figure 6 is the schematic diagram of the structure of the third positioning bracket in the present invention. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0022] In order to make the objectives, contents and advantages of the present invention clearer, the following further describes in detail the specific embodiments of the present invention with reference to the drawings and embodiments.

[0023] This embodiment provides a welding positioning device for an unmanned aerial vehicle engine pipe support, and its structure is as Figures 1 to 3 shown, including a first positioning bracket 1, a second positioning bracket 2 and a third positioning bracket 3, which are respectively used to accurately position the first pipe 4, the second pipe 5 and the third pipe 6 of the engine pipe support. Among them, the first positioning bracket 1 is located at the front of the entire positioning device and is used to position the first pipe 4 of the engine support. The second positioning bracket 2 is located at the upper rear side of the first positioning bracket 1 and is used to position the second pipe 5 of the engine support. The third positioning bracket 3 is located at the lower rear side of the first positioning bracket 1, and the second positioning bracket 2 is above it, and is used to position the third pipe 6 of the engine support. The entire positioning device positions and fastens the first pipe 4, the second pipe 5 and the third pipe 6, so that the mutual positioning accuracy requirements are formed between the pipes, meeting the accuracy control and dimensional requirements of the engine support, and ensuring the reliable assembly of the engine.

[0024] As Figure 4As shown in the figure, the first positioning bracket 1 mainly includes a first cross beam 1-1, a first longitudinal beam 1-2 and a reinforcing rib 1-3. Among them, the two first longitudinal beams 1-2 are fixedly connected to both ends of the first cross beam 1-1. The rear end of the first longitudinal beam 1-2 is fixedly connected to the support rod 3-2 of the third positioning bracket 3. The reinforcing rib 1-3 is connected between the first longitudinal beam 1-2 and the support rod 3-2. A positioning attachment seat is installed at the front end of each first longitudinal beam 1-2, and a bolt 7 and a nut 8 are arranged on each positioning attachment seat. When positioning, the bolt 7 passes through the positioning attachment seat and penetrates the pin hole of the first pipe body 4, and after connecting the first longitudinal beam 1-2 with the first pipe body 4, it is tightened and fixed by the nut 8.

[0025] As Figure 5 shown in the figure, the second positioning bracket 2 mainly includes a second cross beam 2-1. Among them, the second cross beam 2-1 is fixedly connected to the tops of the two support rods 3-2 of the third positioning bracket 3. Positioning attachment seats are installed at both ends of the second cross beam 2-1, and a bolt 7 and a nut 8 are arranged on each positioning attachment seat. When positioning, the bolt 7 passes through the positioning attachment seat and penetrates the pin hole of the second pipe body 5, and after connecting the second cross beam 2-1 with the second pipe body 5, it is tightened and fixed by the nut 8.

[0026] As Figure 6 shown in the figure, the third positioning bracket 3 mainly includes a third cross beam 3-1 and a support rod 3-2. Among them, the third cross beam 3-1 is fixedly connected to the bottoms of the two support rods 3-2. Positioning attachment seats are installed at both ends of the third cross beam 3-1, and a bolt 7 and a nut 8 are arranged on each positioning attachment seat. When positioning, the bolt 7 passes through the positioning attachment seat and penetrates the pin hole of the third pipe body 6, and after connecting the third cross beam 3-1 with the third pipe body 6, it is tightened and fixed by the nut 8.

[0027] When using the welding positioning device for the drone engine pipe body bracket of the present invention, the first pipe body 4, the second pipe body 5 and the third pipe body 6 are respectively positioned and fixed by using bolts and nuts. Check whether the mating parts of each pipe body and the engine bracket welding positioning device are closely fitted. After confirming that there is no error, carry out spot-fixed positioning welding and complete the welding. Since the basic components of the drone body are pipe bodies, each pipe body passes through the pin with holes to form the assembly base point of the engine. Using bolts and nuts to penetrate the pin holes of the pipe bodies to position and fasten the pipe bodies can ensure the positioning accuracy of the engine assembly base point and the reliability of the positioning method. According to the correlation between the pipe bodies of the drone bracket, the engine bracket welding positioning device can combine each pipe body to form an accurate positioning of the bracket.

[0028] The above are only the preferred embodiments of the present invention. It should be noted that for those of ordinary skill in the art, without departing from the technical principle of the present invention, several improvements and deformations can still be made, and these improvements and deformations should also be regarded as the protection scope of the present invention.

Claims

1. A welding positioning device for an engine pipe bracket of a drone, characterized in that, The welding positioning device includes a first positioning bracket, a second positioning bracket, and a third positioning bracket, which are respectively used to accurately position the first pipe body, the second pipe body, and the third pipe body of the engine pipe body bracket. Among them, the first positioning bracket is located at the front of the entire positioning device and is used to position the first pipe body of the engine bracket. The second positioning bracket is located at the upper rear side of the first positioning bracket and is used to position the second pipe body of the engine bracket. The third positioning bracket is located at the lower rear side of the first positioning bracket, and the second positioning bracket is above the third positioning bracket and is used to position the third pipe body of the engine bracket. The entire positioning device forms the mutual positioning accuracy requirements between the pipe bodies through the positioning and fastening of the first pipe body, the second pipe body, and the third pipe body, meeting the accuracy control and dimensional requirements of the engine bracket. The first positioning bracket includes a first cross beam and a first longitudinal beam. Two first longitudinal beams are fixedly connected to both ends of the first cross beam. The rear end of the first longitudinal beam is fixedly connected to the support rod of the third positioning bracket. A positioning attachment seat is installed at the front end of each first longitudinal beam. A bolt and a nut are provided on each positioning attachment seat. During positioning, the bolt passes through the positioning attachment seat and penetrates the pin hole of the first pipe body, and after connecting the first longitudinal beam and the first pipe body, it is tightened and fixed with a nut. The second positioning bracket includes a second cross beam, which is fixedly connected to the tops of the two support rods of the third positioning bracket. Positioning attachment seats are installed at both ends of the second cross beam. A bolt and a nut are provided on each positioning attachment seat. During positioning, the bolt passes through the positioning attachment seat and penetrates the pin hole of the second pipe, and after connecting the second cross beam and the second pipe body, it is tightened and fixed with a nut. The third positioning bracket includes a third cross beam and support rods. The third cross beam is fixedly connected to the bottoms of the two support rods. Positioning attachment seats are installed at both ends of the third cross beam. A bolt and a nut are provided on each positioning attachment seat. During positioning, the bolt passes through the positioning attachment seat and penetrates the pin hole of the third pipe body, and after connecting the third cross beam and the third pipe body, it is tightened and fixed with a nut. A reinforcing rib is connected between the first longitudinal beam and the support rod.

2. The welding positioning device according to claim 1, wherein The first cross beam and the first longitudinal beam are welded and connected.

3. The welding positioning device according to claim 1, characterized in that, The third cross beam and the support rods are welded and connected.

4. The welding positioning device according to claim 1, wherein The positioning attachment seat is welded to the front end of the first longitudinal beam.

5. The welding positioning device according to claim 1, characterized in that, The positioning attachment seats are welded to both ends of the second cross beam.

6. The welding positioning device according to claim 1, characterized in that, The positioning attachment seats are welded to both ends of the third cross beam.

Citation Information

Patent Citations

  • Unmanned aerial vehicle engine pipe body support welding positioning device

    CN219852904U

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