CN220549213U - Satellite communication navigation module base of small unmanned aerial vehicle - Google Patents
Satellite communication navigation module base of small unmanned aerial vehicle Download PDFInfo
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- CN220549213U CN220549213U CN202322256842.0U CN202322256842U CN220549213U CN 220549213 U CN220549213 U CN 220549213U CN 202322256842 U CN202322256842 U CN 202322256842U CN 220549213 U CN220549213 U CN 220549213U
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- unmanned aerial
- aerial vehicle
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- 238000004891 communication Methods 0.000 title claims abstract description 65
- 239000011810 insulating material Substances 0.000 claims description 4
- 230000007423 decrease Effects 0.000 claims description 3
- 230000005288 electromagnetic effect Effects 0.000 abstract description 5
- 238000009434 installation Methods 0.000 description 4
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a satellite communication navigation module base of a small unmanned aerial vehicle. The satellite communication navigation system comprises a main body arranged on the outer side of an unmanned aerial vehicle shell, wherein one end of the main body is connected with the unmanned aerial vehicle shell, and the other end of the main body is used for installing a satellite communication navigation module. According to the utility model, the satellite communication navigation module connected with the main body is arranged outside the unmanned aerial vehicle shell through the main body, so that the problem that the satellite communication navigation module is shielded by the unmanned aerial vehicle shell is avoided, and meanwhile, the interference of the electromagnetic effect of the unmanned aerial vehicle on the work of the satellite communication navigation module is reduced; the device has simple structure and convenient use.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a satellite communication navigation module base of a small unmanned aerial vehicle.
Background
Most of the satellite communication navigation modules on the small unmanned aerial vehicle in the market are arranged inside the unmanned aerial vehicle shell. The satellite communication navigation module is generally integrated on a motherboard built in the unmanned aerial vehicle casing in an integrated manner.
After the satellite communication navigation module is arranged in the unmanned aerial vehicle shell in the mode, the satellite searching rate of the satellite communication navigation module can be reduced due to the shielding of the unmanned aerial vehicle shell, and the problems of low positioning precision and unstable flight attitude of the unmanned aerial vehicle are caused; meanwhile, electromagnetic effects caused by current of the unmanned aerial vehicle can also interfere with the satellite searching rate of the satellite communication navigation module.
Disclosure of Invention
Aiming at the problems existing in the prior art, the utility model aims to provide a satellite communication navigation module base of a small unmanned aerial vehicle, so as to solve the problems that the satellite communication navigation module base is built in a shell of the unmanned aerial vehicle in the prior art, is easy to be interfered by electromagnetic effects caused by currents of the shell of the unmanned aerial vehicle and the unmanned aerial vehicle, and influences the satellite searching rate of the satellite communication navigation module.
The utility model provides a small-size unmanned aerial vehicle satellite communication navigation module base, is including setting up in the main part in the unmanned aerial vehicle casing outside, main part one end with the unmanned aerial vehicle casing is connected, and the other end is used for installing satellite communication navigation module.
Further, one end of the main body is connected with a mounting platform, and the mounting platform is used for being connected with the satellite communication navigation module.
Further, the other end of the main body is connected with a clamp, and the clamp is used for being connected with the unmanned aerial vehicle shell; the clamp pass through the fastener with unmanned aerial vehicle casing fastening connection.
Further, a positioning groove for installing the satellite communication navigation module is formed in one end, connected with the installation platform, of the main body.
Further, the main part middle part is provided with the wiring passageway, wiring passageway one end is to being close to unmanned aerial vehicle casing direction extends, and the other end is to being close to satellite communication navigation module direction extends.
Further, the body is a tubular structure.
Further, the body is made of an insulating material.
Further, the outer diameter of the main body gradually decreases away from the direction of the unmanned aerial vehicle shell.
Further, the clamp is provided with a bolt hole; the fastener is a bolt.
Further, the bolt is locked by adopting double nuts.
According to the utility model, the satellite communication navigation module connected with the main body is arranged outside the unmanned aerial vehicle shell through the main body, so that the problem that the satellite communication navigation module is shielded by the unmanned aerial vehicle shell is avoided, and meanwhile, the interference of the electromagnetic effect of the unmanned aerial vehicle on the work of the satellite communication navigation module is reduced; the device has simple structure and convenient use.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings that are needed in the description of the embodiments or the prior art will be briefly described, and it is obvious that the drawings in the description below are some embodiments of the present utility model, and other drawings can be obtained according to the drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of the overall structure of an embodiment of the present utility model;
FIG. 2 is a front view of an embodiment of the present utility model;
fig. 3 is a side view of an embodiment of the present utility model.
Reference numerals illustrate:
1. a main body; 101. a positioning groove; 102. a wiring channel;
2. a clamp; 201. bolt holes;
3. and (5) installing a platform.
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 some, but not all embodiments of the utility model. The terms "mounted," "connected," and "connected" are to be construed broadly unless otherwise specifically indicated and defined. For ease of description, the terms "vertical," "horizontal," "left," "right," "upper," "lower," "inner," "outer," "bottom," and the like as used herein refer to an orientation or positional relationship based on that shown in the drawings, merely for ease of description and to simplify the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be configured and operated in a particular orientation, and thus are not to be construed as limiting the present application.
The embodiments of the present utility model and the features of the embodiments may be combined with each other without any conflict. 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.
The utility model provides a unmanned aerial vehicle satellite communication navigation module base as shown in fig. 1-3, is including setting up in main part 1, clamp 2 and the mounting platform 3 in the unmanned aerial vehicle casing outside, and the clamp 2 of main part 1 one end is used for being connected with the unmanned aerial vehicle casing, and the mounting platform 3 of the other end is used for installing satellite communication navigation module.
In the embodiment, the satellite communication navigation module connected with the main body 1 is arranged outside the unmanned aerial vehicle shell through the mounting platform 3 at one end of the main body, and a certain distance is kept between the satellite communication navigation module and the unmanned aerial vehicle shell, so that the problem that the satellite communication navigation module is shielded by the unmanned aerial vehicle shell is avoided; meanwhile, a certain distance is kept between the satellite communication navigation module and the power supply and other equipment of the unmanned aerial vehicle, so that the interference of electromagnetic effects of the power supply and other equipment of the unmanned aerial vehicle on the operation of the satellite communication navigation module is reduced; the device has simple structure and convenient use, effectively improves the service performance and reliability of the satellite communication navigation module, and ensures the normal operation of the navigation and communication functions of the satellite communication navigation module.
One end of the main body 1 is connected with a mounting platform 3 which is used for being connected with a satellite communication navigation module.
In this embodiment, the setting of the installation platform 3 can install the satellite communication navigation module simply and conveniently, and the structure is simple, and convenient to use.
The other end of the main body 1 is provided with a clamp 2 for connecting with the shell of the unmanned aerial vehicle; the clamp 2 is connected with the unmanned aerial vehicle casing through the fastener fastening.
In this embodiment, clamp 2 can be through the horn locking on fastener with main part 1 and unmanned aerial vehicle casing, and is fixed reliable, easy to assemble and dismantlement.
The main body 1 is provided with a positioning groove 101 for installing a satellite communication navigation module at one end connected with the installation platform 3. Wherein the opening direction of the positioning groove 101 points to the mounting platform 3.
In this embodiment, a positioning block adapted to the positioning slot 101 is disposed at the bottom of the satellite communication navigation module, and the positioning block can slide downward along the positioning slot 101 and cooperate with the positioning slot 101 to mount the satellite communication navigation module, and the positioning slot 101 and the positioning block are disposed to facilitate the installation of the satellite communication navigation module.
The middle part of main part 1 is provided with wiring passageway 102, and wiring passageway 102 one end extends to the direction that is close to the unmanned aerial vehicle casing, and the other end extends to the direction that is close to satellite communication navigation module.
In this embodiment, the wiring channel 102 is configured to be used for placing the wire harness for electrical connection when the satellite communication navigation module is connected with other devices on the unmanned aerial vehicle, so that the main body 1 can hide the wire harness, and the wire harness can be protected to a certain extent while being conveniently and aesthetically stored, thereby ensuring normal use of the unmanned aerial vehicle.
The body 1 is of tubular construction.
In this embodiment, the tubular structure includes a round tube or other tubular type in the prior art, and has a simple structure and is convenient to manufacture.
The body 1 is made of an insulating material.
In this embodiment, the insulating material can avoid interference caused by the leakage phenomenon.
The outer diameter of the main body 1 gradually decreases away from the unmanned aerial vehicle casing.
In this embodiment, the main body 1 has a generally conical tubular structure, and has less material loss, higher structural strength and more durability.
The clamp 2 is provided with two bolt holes 201 which are horizontally arranged at intervals; the fastener is a bolt, and the bolt cooperates with bolt hole 201 to lock unmanned aerial vehicle.
In this embodiment, adopt the bolt to connect, simple structure, easy to assemble and dismantlement.
The bolt is locked by double nuts.
In this embodiment, the double nut locking is used for locking for guarantee unmanned aerial vehicle's normal use.
The base of the satellite communication navigation module of the unmanned aerial vehicle is used for installing the satellite communication navigation module of the unmanned aerial vehicle outside an unmanned aerial vehicle shell, and isolating the interference of the magnetic field generated by the unmanned aerial vehicle on the satellite communication navigation module by blocking the conducting path of the magnetic field, so that the unmanned aerial vehicle can maintain a more stable posture in the flying process.
Meanwhile, the signal shielding problem of the unmanned aerial vehicle shell to the satellite communication navigation module is avoided. Unmanned aerial vehicle enclosures often have a shielding effect that may affect signal transmission between the satellite communication navigation module and the satellite. Through setting up satellite communication navigation module in the unmanned aerial vehicle casing outside, make satellite communication navigation module keep certain interval with the unmanned aerial vehicle casing, can reduce the interference of unmanned aerial vehicle casing to satellite communication navigation module signal, ensure the normal transmission of communication and navigation signal.
It is apparent that the above examples are given by way of illustration only and are not limiting of the embodiments. Other variations or modifications of the above teachings will be apparent to those of ordinary skill in the art. It is not necessary here nor is it exhaustive of all embodiments. While still being apparent from variations or modifications that may be made by those skilled in the art are within the scope of the utility model.
Claims (10)
1. The utility model provides a small-size unmanned aerial vehicle satellite communication navigation module base, its characterized in that, including setting up in the main part in the unmanned aerial vehicle casing outside, main part one end with the unmanned aerial vehicle casing is connected, and the other end is used for installing satellite communication navigation module.
2. The unmanned aerial vehicle satellite communication navigation module base of claim 1, wherein one end of the main body is connected with a mounting platform, and the mounting platform is used for being connected with the satellite communication navigation module.
3. The base of a satellite communication navigation module of claim 2, wherein a clip is connected to the other end of the main body, and the clip is configured to connect with the unmanned aerial vehicle housing; the clamp pass through the fastener with unmanned aerial vehicle casing fastening connection.
4. The unmanned aerial vehicle satellite communication navigation module base of claim 2, wherein the end of the main body to which the mounting platform is connected is provided with a positioning slot for mounting the satellite communication navigation module.
5. The base of claim 1, wherein a wiring channel is provided in the middle of the main body, and one end of the wiring channel extends in a direction close to the casing of the unmanned aerial vehicle, and the other end extends in a direction close to the satellite communication navigation module.
6. The unmanned aerial vehicle satellite communication navigation module base of any of claims 1-5, wherein the body is tubular in structure.
7. The unmanned aerial vehicle satellite communication navigation module base of claim 6, wherein the body is made of an insulating material.
8. The unmanned aerial vehicle satellite communication navigation module base of claim 6, wherein the outer diameter of the body decreases progressively away from the unmanned aerial vehicle housing.
9. The unmanned aerial vehicle satellite communication navigation module base of claim 3, wherein the clip is provided with bolt holes; the fastener is a bolt.
10. The unmanned aerial vehicle satellite communication navigation module base of claim 9, wherein the bolts are locked with double nuts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322256842.0U CN220549213U (en) | 2023-08-22 | 2023-08-22 | Satellite communication navigation module base of small unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322256842.0U CN220549213U (en) | 2023-08-22 | 2023-08-22 | Satellite communication navigation module base of small unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220549213U true CN220549213U (en) | 2024-03-01 |
Family
ID=90009823
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322256842.0U Active CN220549213U (en) | 2023-08-22 | 2023-08-22 | Satellite communication navigation module base of small unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220549213U (en) |
-
2023
- 2023-08-22 CN CN202322256842.0U patent/CN220549213U/en active Active
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