CN221087348U - Unmanned aerial vehicle radome fairing side system hole frock - Google Patents

Unmanned aerial vehicle radome fairing side system hole frock Download PDF

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Publication number
CN221087348U
CN221087348U CN202322882302.3U CN202322882302U CN221087348U CN 221087348 U CN221087348 U CN 221087348U CN 202322882302 U CN202322882302 U CN 202322882302U CN 221087348 U CN221087348 U CN 221087348U
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base
fixing
aerial vehicle
unmanned aerial
fixing base
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CN202322882302.3U
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赖秀芳
舒宏杰
张国勤
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Jiangxi Xinhang Aviation Technology Co ltd
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Jiangxi Xinhang Aviation Technology Co ltd
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Abstract

The utility model discloses an unmanned aerial vehicle fairing side edge hole making tool which comprises a base and a fixed base, wherein the fixed base comprises a first fixed base, a second fixed base, a third fixed base, a fourth fixed base and a fifth fixed base, the base comprises one side of the base, two sides of the base, three sides of the base and four sides of the base, a first gap is formed between the first fixed base and the second fixed base, a second gap is formed between the second fixed base and the third fixed base, a third gap is formed between the third fixed base and the fourth fixed base, a fourth gap is formed between the fourth fixed base and the fifth fixed base, and the unmanned aerial vehicle fairing performs hole making operation on the surface of the unmanned aerial vehicle fairing through the first gap, the second gap, the third gap and the fourth gap. According to the utility model, through arranging the plurality of fixing seats and the gaps, multidirectional fixing and hole making of the unmanned aerial vehicle fairing can be realized, and the processing efficiency and accuracy are improved.

Description

Unmanned aerial vehicle radome fairing side system hole frock
Technical Field
The utility model relates to the field of tooling equipment, in particular to an unmanned aerial vehicle fairing side edge hole making tooling.
Background
Unmanned aerial vehicle is an aircraft that can fly under unmanned circumstances, and it has extensive application such as military affairs, scientific research, rescue etc.. The design of the exterior of the unmanned aerial vehicle has an important influence on its flight performance, wherein the fairing is a kind of enclosure for reducing air resistance and protecting internal equipment. The shape of the drone fairing is often irregular and, in order to increase its strength and stability, it is necessary to perform a hole making operation on its sides in order to install screws or other connectors.
However, due to the irregular structure of the unmanned aerial vehicle fairing, when the hole making operation is carried out on the side edge of the unmanned aerial vehicle fairing, the unmanned aerial vehicle fairing needs to be fixed in multiple directions so as to ensure the hole making precision and position. The fixing mode not only needs a plurality of tools and operators, but also can increase the time and cost for making holes, and reduce the processing efficiency and quality. Therefore, how to design a simple, quick and accurate unmanned aerial vehicle radome side hole making tool is a technical problem to be solved in the prior art.
Disclosure of utility model
The utility model aims to solve the technical problems, thereby providing an unmanned aerial vehicle fairing side edge hole making tool;
in order to solve the technical problems, the following technical scheme is provided:
The utility model provides an unmanned aerial vehicle fairing side edge hole making tool,
Including base, fixing base, the fixing base sets up on the base, the fixing base includes first fixing base, second fixing base, third fixing base, fourth fixing base, fifth fixing base, the base includes base one side, base two sides, base trilateral, base four sides, first fixing base, second fixing base, third fixing base all interval sets up in proper order on the base one side, the fourth fixing base sets up on the base two sides, the fifth fixing base sets up on the base three sides, first fixing base with form first clearance between the second fixing base, the second fixing base with form the second clearance between the third fixing base, the third fixing base with form the third clearance between the fourth fixing base, form the fourth clearance between the fourth fixing base, form between first fixing base, second fixing base, third fixing base, fourth fixing base, the fifth fixing base and place the space, unmanned aerial vehicle fairing is placed on the base through place the space, the unmanned aerial vehicle fairing warp first clearance, second clearance, third clearance, fourth clearance make its clearance surface to make the hole.
Optionally, the first fixing base, the second fixing base, the third fixing base, the fourth fixing base, the fifth fixing base face the surface of unmanned aerial vehicle radome fairing all is provided with the inoxidizing coating, the inoxidizing coating is used for protecting the surface of unmanned aerial vehicle radome fairing.
Optionally, the first fixing seat, the second fixing seat, the third fixing seat, the fourth fixing seat and the fifth fixing seat are all integrally formed with the base, or the first fixing seat, the second fixing seat, the third fixing seat, the fourth fixing seat and the fifth fixing seat are all welded on the base.
Optionally, the base is provided with a mounting hole, and the base is fixed on the workbench through the mounting hole.
Optionally, the mounting holes are arranged in a plurality of groups, and the plurality of groups of mounting holes are arranged on the base at intervals.
The utility model has the beneficial effects that
According to the tooling disclosed by the application, the unmanned aerial vehicle fairing can be fixed on the base at one time by arranging the plurality of fixing seats and the gaps, and then holes are formed on the side edges of the unmanned aerial vehicle fairing along each gap, so that frequent movement and adjustment are not required, and the processing efficiency is greatly improved.
Drawings
Fig. 1 is a schematic diagram of the assembly of the present utility model with a unmanned aerial vehicle fairing.
Fig. 2 is a schematic structural view of a fairing of an unmanned aerial vehicle according to the present utility model.
Reference numerals illustrate: the device comprises a 1-base, a 2-first fixing seat, a 3-second fixing seat, a 4-third fixing seat, a 5-fourth fixing seat, a 6-fifth fixing seat, a 7-base side, an 8-base two sides, a 9-base three sides, a 10-base four sides, an 11-first gap, a 12-second gap, a 13-third gap, a 14-fourth gap, a 15-placing space and a 16-unmanned aerial vehicle fairing.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Examples
As shown in fig. 1-2, the utility model provides an unmanned aerial vehicle fairing side edge hole making tool,
The unmanned aerial vehicle comprises a base 1 and a fixed seat, wherein the fixed seat is arranged on the base 1 and comprises a first fixed seat 2, a second fixed seat 3, a third fixed seat 4, a fourth fixed seat 5 and a fifth fixed seat 6, the base 1 comprises a base side 7, a base two side 8, a base three side 9 and a base four side 10, the first fixed seat 2, the second fixed seat 3 and the third fixed seat 4 are sequentially arranged on the base side 7 at intervals, the fourth fixed seat 5 is arranged on the base two side 8, the fifth fixed seat 6 is arranged on the base three side 9, a first gap 11 is formed between the first fixed seat 2 and the second fixed seat 3, a second gap 12 is formed between the second fixed seat 3 and the third fixed seat 4, a third gap 13 is formed between the third fixed seat 4 and the fourth fixed seat 5, a fourth gap 14 is formed between the fourth fixed seat 5 and the fifth fixed seat 6, a rectifier space 15 is formed between the first fixed seat 2, the second fixed seat 3, the third fixed seat 4 and the fourth fixed seat 5 and the fifth fixed seat 6, a rectifier space 16 is formed between the first fixed seat 4 and the fourth fixed seat 6, and the rectifier space 16 is formed between the rectifier space and the fourth fixed seat 16 and the fourth fixed seat 1 and the unmanned aerial vehicle through the gap 14;
The surfaces of the first fixing seat 2, the second fixing seat 3, the third fixing seat 4, the fourth fixing seat 5 and the fifth fixing seat 6 facing the unmanned aerial vehicle fairing 16 are all provided with protective layers, the protective layers are used for protecting the surfaces of the unmanned aerial vehicle fairing 16, and the surfaces of the unmanned aerial vehicle fairing 16 can be protected from being scratched or worn by arranging the protective layers, so that the product quality is improved, and the service life is prolonged;
In the use process, firstly, the unmanned aerial vehicle fairing 16 is placed on the base 1, so that the unmanned aerial vehicle fairing is placed in a placing space 15 formed among the first fixing seat 2, the second fixing seat 3, the third fixing seat 4, the fourth fixing seat 5 and the fifth fixing seat 6, and the side edges of the unmanned aerial vehicle fairing 16 are aligned with the first gap 11, the second gap 12, the third gap 13 and the fourth gap 14;
The base 1 is fixed on the workbench through the mounting holes by bolts or other fixing pieces, so that the base is stable and motionless;
And (3) using a punching machine or other hole forming equipment to perform hole forming operation on the side edge of the unmanned aerial vehicle fairing 16 along the first gap 11, the second gap 12, the third gap 13 and the fourth gap 14, wherein the hole forming position and size can be adjusted according to requirements.
After the hole is formed, the bolts or other fixing parts are disassembled, the unmanned aerial vehicle fairing 16 is taken down from the base 1, and the quality and effect of the hole are checked;
if necessary, the above steps can be repeated, and the other sides of the unmanned aerial vehicle fairing 16 can be subjected to hole making operation;
According to the utility model, by arranging a plurality of fixing seats and gaps, multidirectional fixing and hole making of the unmanned aerial vehicle fairing 16 can be realized, and the processing efficiency and accuracy are improved;
Specific:
From the aspect of processing efficiency, because the shape of the unmanned aerial vehicle fairing 16 is irregular, if a traditional single fixing mode is used, the position and angle of the unmanned aerial vehicle fairing 16 need to be adjusted repeatedly so as to hole different sides of the unmanned aerial vehicle fairing, and thus a great deal of time and manpower can be wasted. According to the tooling disclosed by the application, the unmanned aerial vehicle fairing 16 can be fixed on the base 1 at one time by arranging the plurality of fixing seats and the gaps, and then holes are formed on the side edges of the unmanned aerial vehicle fairing along the gaps, so that frequent movement and adjustment are not required, and the processing efficiency is greatly improved.
From the aspect of processing precision, because the structure of the unmanned aerial vehicle fairing 16 is complex, if a traditional single fixing mode is used, the unmanned aerial vehicle fairing 16 may shake or deviate in the hole making process, and the hole making position and size are affected. The tool provided by the application can firmly fix the unmanned aerial vehicle fairing 16 on the base 1 by arranging a plurality of fixing seats and gaps, so that deformation or displacement can not occur in the hole making process, and the hole making precision and quality are improved.
In terms of processing range, because the shape of the unmanned aerial vehicle fairing 16 is various, if a traditional single fixing mode is used, part of side edges can not be drilled, or special hole-making equipment is required, so that processing difficulty and cost are increased. The tooling provided by the application can adapt to unmanned aerial vehicle fairings 16 with different shapes by arranging a plurality of fixing seats and gaps, holes are formed on each side edge of the unmanned aerial vehicle fairings, the tooling or equipment does not need to be replaced or adjusted, and the processing range and flexibility are increased.
The base 1 is provided with mounting holes, the base 1 is fixed on the workbench through the mounting holes, the mounting holes are arranged into a plurality of groups, the mounting holes are arranged on the base 1 at intervals, and the base 1 can be conveniently fixed on the workbench through the mounting holes, so that the stability and the safety of the tool are improved.
The first fixing seat 2, the second fixing seat 3, the third fixing seat 4, the fourth fixing seat 5 and the fifth fixing seat 6 are all arranged with the base 1 into an integrated structure, or the first fixing seat 2, the second fixing seat 3, the third fixing seat 4, the fourth fixing seat 5 and the fifth fixing seat 6 are all welded on the base 1, and the cost and the weight of the tool can be reduced by adopting the integrated structure or the welded structure, and the reliability and the portability of the tool are improved.
Finally, it should be noted that: the foregoing description is only illustrative of the preferred embodiments of the present utility model, and although the present utility model has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present utility model.

Claims (5)

1. An unmanned aerial vehicle radome fairing side edge hole making tool is characterized in that,
Including base, fixing base, the fixing base sets up on the base, the fixing base includes first fixing base, second fixing base, third fixing base, fourth fixing base, fifth fixing base, the base includes base one side, base two sides, base trilateral, base four sides, first fixing base, second fixing base, third fixing base all interval sets up in proper order on the base one side, the fourth fixing base sets up on the base two sides, the fifth fixing base sets up on the base three sides, first fixing base with form first clearance between the second fixing base, the second fixing base with form the second clearance between the third fixing base, the third fixing base with form the third clearance between the fourth fixing base, form the fourth clearance between the fourth fixing base, form between first fixing base, second fixing base, third fixing base, fourth fixing base, the fifth fixing base and place the space, unmanned aerial vehicle fairing is placed on the base through place the space, the unmanned aerial vehicle fairing warp first clearance, second clearance, third clearance, fourth clearance make its clearance surface to make the hole.
2. The unmanned aerial vehicle radome side hole-making tool of claim 1, wherein,
The first fixing base, the second fixing base, the third fixing base, the fourth fixing base and the fifth fixing base face the surface of the unmanned aerial vehicle fairing is provided with a protective layer, and the protective layer is used for protecting the surface of the unmanned aerial vehicle fairing.
3. The unmanned aerial vehicle radome side hole-making tool of claim 2, wherein,
The first fixing seat, the second fixing seat, the third fixing seat, the fourth fixing seat and the fifth fixing seat are all arranged with the base to form an integrated structure, or the first fixing seat, the second fixing seat, the third fixing seat, the fourth fixing seat and the fifth fixing seat are all welded on the base.
4. The unmanned aerial vehicle radome side hole-making tool of claim 1, wherein,
The base is provided with a mounting hole, and the base is fixed on the workbench through the mounting hole.
5. The unmanned aerial vehicle radome side hole-making tool of claim 4, wherein,
The mounting holes are arranged in a plurality of groups, and the plurality of groups of mounting holes are arranged on the base at intervals.
CN202322882302.3U 2023-10-26 2023-10-26 Unmanned aerial vehicle radome fairing side system hole frock Active CN221087348U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322882302.3U CN221087348U (en) 2023-10-26 2023-10-26 Unmanned aerial vehicle radome fairing side system hole frock

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322882302.3U CN221087348U (en) 2023-10-26 2023-10-26 Unmanned aerial vehicle radome fairing side system hole frock

Publications (1)

Publication Number Publication Date
CN221087348U true CN221087348U (en) 2024-06-07

Family

ID=91303955

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322882302.3U Active CN221087348U (en) 2023-10-26 2023-10-26 Unmanned aerial vehicle radome fairing side system hole frock

Country Status (1)

Country Link
CN (1) CN221087348U (en)

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