CN219679126U - Flight data transmission module - Google Patents
Flight data transmission module Download PDFInfo
- Publication number
- CN219679126U CN219679126U CN202321180287.1U CN202321180287U CN219679126U CN 219679126 U CN219679126 U CN 219679126U CN 202321180287 U CN202321180287 U CN 202321180287U CN 219679126 U CN219679126 U CN 219679126U
- Authority
- CN
- China
- Prior art keywords
- data transmission
- transmission module
- shaped
- module body
- wall
- Prior art date
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- 230000005540 biological transmission Effects 0.000 title claims abstract description 54
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 15
- 239000000741 silica gel Substances 0.000 claims abstract description 15
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 15
- 239000011111 cardboard Substances 0.000 claims abstract description 8
- 230000005855 radiation Effects 0.000 claims abstract description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 230000017525 heat dissipation Effects 0.000 abstract description 10
- 239000006185 dispersion Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 description 7
- 238000009434 installation Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 230000009286 beneficial effect Effects 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
- 238000004080 punching Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
Abstract
The utility model belongs to the technical field of data transmission, and particularly relates to a flight data transmission module, which comprises a data transmission module body, wherein an L-shaped shield is sleeved on the outer wall of the data transmission module body, an L-shaped silica gel heat conduction pad is arranged at the top end of the inner wall of the L-shaped shield, limit clamping holes are symmetrically formed in the bottoms of two sides of the inner wall of the L-shaped shield, L-shaped limit clamping plates penetrate through the two corresponding limit clamping holes, and a plurality of heat dissipation fins are arranged at the top end of the L-shaped shield. Through the cooperation of spacing card hole and the spacing cardboard of L type use, can fix L type guard shield, through the use of L type guard shield, L type silica gel heat conduction pad and heat radiation fin, can improve the heat dispersion of data transmission module body, avoid the overheated phenomenon of data transmission module body in the use to appear, can protect the electrical components of data transmission module body simultaneously, the steady use of data transmission module body of being convenient for.
Description
Technical Field
The utility model belongs to the technical field of data transmission, and particularly relates to a flight data transmission module.
Background
In the remote control process of the unmanned aerial vehicle, real-time signal transmission is needed, a flight data transmission module is needed in the process, a heat dissipation device is not generally used in the using process (such as an HM-TRP 868MHzAPM flight control wireless data transmission module) of the flight data transmission module on the market, and when the unmanned aerial vehicle continuously operates, the data transmission module is easy to overheat, so that the data transmission efficiency is affected.
Disclosure of Invention
In order to solve the problems in the prior art, the utility model provides the flight data transmission module, and the heat dissipation performance of the data transmission module body can be improved through the use of the L-shaped shield, the L-shaped silica gel heat conduction pad and the heat dissipation fins, so that the phenomenon that the data transmission module body is overheated in the use process is avoided, and meanwhile, the electric elements of the data transmission module body can be protected, so that the stable use of the data transmission module body is facilitated.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a flight data transmission module, includes the data transmission module body, data transmission module body outer wall cover is equipped with L type guard shield, L type silica gel heat conduction pad is installed on L type guard shield inner wall top, spacing card hole has all been seted up to L type guard shield inner wall both sides bottom symmetry, two correspond the setting spacing card hole is inside to have all run through L type spacing cardboard, L type guard shield top is provided with a plurality of heat radiation fins.
As a preferable technical scheme of the flight data transmission module, the L-shaped shield is formed by stamping an aluminum sheet.
As a preferable technical scheme of the flight data transmission module, the cross section size of the L-shaped silica gel heat conduction pad is matched with the cross section size of the top end of the inner wall of the L-shaped shield.
As a preferable technical scheme of the flight data transmission module, the L-shaped limiting clamping plate is made of PP plastic.
As a preferable technical scheme of the flight data transmission module, the longitudinal section size of the L-shaped limiting clamping plate is the same as the longitudinal section size of the limiting clamping hole.
As an optimal technical scheme of the flight data transmission module, one side of the L-shaped limiting clamping plate is provided with a pointed head, and one side of the inner wall of the L-shaped limiting clamping plate is provided with an arc-shaped opening.
Compared with the prior art, the utility model has the beneficial effects that:
when the utility model is used, the L-shaped shield can be fixed through the cooperation of the limit clamping holes and the L-shaped limit clamping plates, and the heat dissipation performance of the data transmission module body can be improved through the use of the L-shaped shield, the L-shaped silica gel heat conduction pad and the heat dissipation fins, so that the phenomenon that the data transmission module body is overheated in the use process is avoided, meanwhile, the electric elements of the data transmission module body can be protected, and the stable use of the data transmission module body is facilitated.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a view showing the installation effect of the L-shaped limiting clamping plate;
FIG. 3 is an exploded view of the installation of the L-shaped shield of the present utility model.
In the figure: 1. a data transmission module body; 2. an L-shaped shield; 3. l-shaped silica gel heat conducting pad; 4. limiting clamping holes; 5. an L-shaped limiting clamping plate; 6. and the heat dissipation fins.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. 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
Referring to fig. 1-3, the present utility model provides the following technical solutions: the utility model provides a flight data transmission module, including data transmission module body 1, data transmission module body 1 outer wall cover is equipped with L type guard shield 2, L type guard shield 2 comprises the aluminium sheet punching press, L type guard shield 2's production of being convenient for is made, L type silica gel heat conduction pad 3 is installed on L type guard shield 2 inner wall top, L type silica gel heat conduction pad 3's cross section size and L type guard shield 2 inner wall top cross section size looks adaptation, L type silica gel heat conduction pad 3's installation of being convenient for uses, spacing card hole 4 has all been seted up to L type guard shield 2 inner wall both sides bottom symmetry, the material that two spacing card holes 4 that correspond the setting are inside has all run through L type spacing card board 5,L type spacing card board 5 is PP plastics, L type spacing card board 5's longitudinal section size is the same with spacing card hole 4's longitudinal section size, L type spacing card board 5 one side sets up to the tip, L type spacing card 5 inner wall one side is provided with the arc opening, L type spacing card board 5's of being convenient for install use, L type guard shield 2 top is provided with a plurality of heat dissipation fins 6.
The working principle and the using flow of the utility model are as follows: in the using process, a worker installs the L-shaped silica gel heat conduction pad 3 on the inner wall of the L-shaped shield 2, then the worker moves the L-shaped shield 2 to enable the data transmission module body 1 to enter the L-shaped shield 2 and contact the L-shaped silica gel heat conduction pad 3, then the worker presses between the data transmission module body 1 and the L-shaped shield 2, then the worker installs the L-shaped limiting clamping plate 5 to fix the L-shaped shield 2, and through the use of the L-shaped shield 2, the L-shaped silica gel heat conduction pad 3 and the heat dissipation fins 6, the heat dissipation performance of the data transmission module body 1 can be improved, the phenomenon that the data transmission module body 1 is overheated in the using process is avoided, meanwhile, the electric appliance elements of the data transmission module body 1 can be protected, and the stable use of the data transmission module body 1 is facilitated.
Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.
Claims (6)
1. A flight data transmission module comprising a data transmission module body (1), characterized in that: the utility model discloses a data transmission module, including data transmission module body (1), L type guard shield (2) are equipped with to data transmission module body (1) outer wall cover, L type silica gel heat conduction pad (3) are installed on L type guard shield (2) inner wall top, spacing card hole (4) have all been seted up to L type guard shield (2) inner wall both sides bottom symmetry, two correspond the setting spacing card hole (4) are inside all to run through there is L type spacing cardboard (5), L type guard shield (2) top is provided with a plurality of heat radiation fins (6).
2. A flight data transmission module as claimed in claim 1, wherein: the L-shaped shield (2) is formed by stamping an aluminum sheet.
3. A flight data transmission module as claimed in claim 1, wherein: the cross section size of the L-shaped silica gel heat conduction pad (3) is matched with the cross section size of the top end of the inner wall of the L-shaped shield (2).
4. A flight data transmission module as claimed in claim 1, wherein: the L-shaped limiting clamping plate (5) is made of PP plastic.
5. A flight data transmission module as claimed in claim 1, wherein: the longitudinal section size of the L-shaped limiting clamping plate (5) is the same as the longitudinal section size of the limiting clamping hole (4).
6. A flight data transmission module as claimed in claim 1, wherein: one side of the L-shaped limiting clamping plate (5) is provided with a pointed end, and one side of the inner wall of the L-shaped limiting clamping plate (5) is provided with an arc-shaped opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321180287.1U CN219679126U (en) | 2023-05-17 | 2023-05-17 | Flight data transmission module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321180287.1U CN219679126U (en) | 2023-05-17 | 2023-05-17 | Flight data transmission module |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219679126U true CN219679126U (en) | 2023-09-12 |
Family
ID=87922098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321180287.1U Active CN219679126U (en) | 2023-05-17 | 2023-05-17 | Flight data transmission module |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219679126U (en) |
-
2023
- 2023-05-17 CN CN202321180287.1U patent/CN219679126U/en active Active
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| GR01 | Patent grant |