CN214897420U - Flight instrument liquid crystal display module - Google Patents
Flight instrument liquid crystal display module Download PDFInfo
- Publication number
- CN214897420U CN214897420U CN202120620942.5U CN202120620942U CN214897420U CN 214897420 U CN214897420 U CN 214897420U CN 202120620942 U CN202120620942 U CN 202120620942U CN 214897420 U CN214897420 U CN 214897420U
- Authority
- CN
- China
- Prior art keywords
- support
- liquid crystal
- display module
- crystal display
- display screen
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000004973 liquid crystal related substance Substances 0.000 title claims abstract description 17
- 239000007769 metal material Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 8
- 238000010586 diagram Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
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Abstract
The utility model discloses a flight instrument liquid crystal display module, comprising a base plate, surface mounting has the cylindric lock of being no less than one on the bottom plate, the spring is installed to the disc outside the cylindric lock, the support is installed to the cylindric lock upper end, the cylindric lock upwards wears out the support, just the dop is installed on the cylindric lock top, the cylindric lock with support sliding connection, be provided with the recess in the support. Has the advantages that: utilize the fan to dispel the heat to the display screen, make the radiating effect of display screen better, it is more convenient to use, cushions the vibrations that the instrument produced through cylindric lock and spring moreover, protection display screen that can be better.
Description
Technical Field
The utility model relates to a liquid crystal display module technical field, concretely relates to flight instrument liquid crystal display module.
Background
Flight instruments are tools for measuring and representing data of an aircraft, which is an essential part of the aircraft, and a pilot can correctly make a judgment according to the data represented by the flight instruments. The flight instrument is used for displaying data and is provided with a liquid crystal display module.
The radiating effect of the existing flight display module is not good, the use is very inconvenient, and the vibration generated by the instrument cannot be buffered in the use process, so that the display module is easy to vibrate, and the protection of the display module is not facilitated.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aerometer liquid crystal display module assembly in order to solve above-mentioned problem, the utility model provides an optimal technical scheme utilizes the fan to dispel the heat to the display screen among a great deal of technical scheme, makes the radiating effect of display screen better, and it is more convenient to use, cushions the vibrations that the instrument produced through cylindric lock and spring moreover, and the protection display screen that can be better is elaborated in detail below.
In order to achieve the above purpose, the utility model provides a following technical scheme:
the utility model provides a flight instrument liquid crystal display module, which comprises a bottom plate, wherein the upper surface of the bottom plate is provided with at least one cylindrical pin, a spring is arranged on the outer circular surface of the cylindrical pin, a bracket is arranged at the upper end of the cylindrical pin, the cylindrical pin extends upwards out of the bracket, and the top end of the cylindrical pin is provided with a chuck, the cylindrical pin is connected with the bracket in a sliding way, the bracket is internally provided with a groove, a display screen is arranged in the groove, less than one fan is arranged on the inner bottom surface of the bracket, at least one hole is arranged on the bottom surface of the bracket, the hole corresponds to the fan, the top end of the bracket is provided with a cover plate which is of a frame-shaped structure, and fastening bolts are arranged on the top surface of the cover plate and penetrate through the cover plate downwards, and the fastening bolts are connected with the support bolts.
Adopt above-mentioned flight instrument liquid crystal display module assembly, utilize the apron will the display screen is fixed in the support in the recess, through fastening bolt will the apron is fixed on the support, in the use, it is right to utilize the fan dispels the heat the display screen, makes the radiating effect of display screen is better, and it is more convenient to use, when the instrument produced vibrations, the cylindric lock is in slide on the support under the spring action, cushion the vibrations that the instrument produced, protection that can be better the display screen.
Preferably, the meshes are installed on two sides of the bracket and made of metal materials.
Preferably, the cover plate is made of rubber.
Preferably, the number of the cylindrical pins is several, and the cylindrical pins are uniformly distributed on the surface of the bottom plate.
Preferably, the display screen is in an elliptical structure.
Preferably, the fan is bolted to the support.
Preferably, a gasket is arranged between the display screen and the bracket.
Has the advantages that: utilize the fan to dispel the heat to the display screen, make the radiating effect of display screen better, it is more convenient to use, cushions the vibrations that the instrument produced through cylindric lock and spring moreover, protection display screen that can be better.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of the present invention;
fig. 2 is a top view of the present invention;
fig. 3 is a schematic structural diagram of the middle support of the present invention.
The reference numerals are explained below:
1. a base plate; 2. a support; 201. a mesh sheet; 202. a groove; 203. a hole; 3. a display screen; 4. fastening a bolt; 5. a cover plate; 6. a cylindrical pin; 601. clamping a head; 7. a spring; 8. a fan.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the technical solutions of the present invention will be described in detail below. It is to be understood that the embodiments described are only some embodiments of the invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, the utility model provides a flight instrument liquid crystal display module, which comprises a bottom plate 1, at least one cylindrical pin 6 is installed on the upper surface of the bottom plate 1, a spring 7 is installed on the outer circular surface of the cylindrical pin 6, a bracket 2 is installed on the upper end of the cylindrical pin 6, the cylindrical pin 6 is upwards passed through the bracket 2, and dop 601 is installed on 6 tops of cylindric lock, cylindric lock 6 and support 2 sliding connection, be provided with recess 202 in the support 2, display screen 3 has been placed in the recess 202, the bottom surface is installed and is less than one fan 8 in the support 2, 2 bottom surfaces of support are provided with and are no less than one hole 203, hole 203 is corresponding with fan 8, apron 5 is installed on 2 tops of support, apron 5 is the frame-shaped structure, fastening bolt 4 is installed to apron 5 top surfaces, fastening bolt 4 runs through apron 5 downwards, and fastening bolt 4 and support 2 bolted connection.
As optional implementation mode, net piece 201 is installed to support 2 both sides, and net piece 201 adopts the metal material to make, sets up like this, makes things convenient for the interior ventilation of support 2 through net piece 201, and the radiating effect is better.
The cover plate 5 is made of rubber materials, so that the display screen 3 can be protected, and the edge of the display screen 3 is prevented from being damaged.
The display screen 3 is of an oval structure, and the display screen 3 is not easy to damage due to the oval design.
Install the gasket between display screen 3 and support 2, set up like this, make display screen 3 fixed more firm.
Adopt above-mentioned structure, utilize apron 5 to fix display screen 3 in the recess 202 of support 2, fix apron 5 on support 2 through fastening bolt 4, in the use, utilize fan 8 to dispel the heat to display screen 3, make display screen 3's radiating effect better, it is more convenient to use, when the instrument produces vibrations, cylindric lock 6 slides on support 2, under spring 7's elastic force effect, the vibrations that produce the instrument are cushioned, protection display screen 3 that can be better.
The above description is only for the specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art can easily think of the changes or substitutions within the technical scope of the present invention, and all should be covered within the protection scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (7)
1. The utility model provides a flight instrument liquid crystal display module which characterized in that: the novel fan support is characterized by comprising a base plate (1), wherein at least one cylindrical pin (6) is arranged on the upper surface of the base plate (1), a spring (7) is arranged on the outer circular surface of the cylindrical pin (6), a support (2) is arranged at the upper end of the cylindrical pin (6), the cylindrical pin (6) upwards penetrates out of the support (2), a clamping head (601) is arranged at the top end of the cylindrical pin (6), the cylindrical pin (6) is in sliding connection with the support (2), a groove (202) is formed in the support (2), a display screen (3) is arranged in the groove (202), less than one fan (8) is arranged on the inner bottom surface of the support (2), at least one hole (203) is formed in the bottom surface of the support (2), the hole (203) corresponds to the fan (8), a cover plate (5) is arranged at the top end of the support (2), and the cover plate (5) is of a frame-shaped structure, fastening bolts (4) are installed on the top surface of the cover plate (5), the fastening bolts (4) penetrate through the cover plate (5) downwards, and the fastening bolts (4) are connected with the support (2) through bolts.
2. The flight instrument liquid crystal display module of claim 1, wherein: the net piece (201) is installed to support (2) both sides, just net piece (201) adopt the metal material to make.
3. The flight instrument liquid crystal display module of claim 1, wherein: the cover plate (5) is made of rubber materials.
4. The flight instrument liquid crystal display module of claim 1, wherein: the number of the cylindrical pins (6) is a plurality, and the cylindrical pins are uniformly distributed on the surface of the bottom plate (1).
5. The flight instrument liquid crystal display module of claim 1, wherein: the display screen (3) is of an oval structure.
6. The flight instrument liquid crystal display module of claim 1, wherein: the fan (8) is connected with the bracket (2) through bolts.
7. The flight instrument liquid crystal display module of claim 1, wherein: and a gasket is arranged between the display screen (3) and the bracket (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120620942.5U CN214897420U (en) | 2021-03-27 | 2021-03-27 | Flight instrument liquid crystal display module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120620942.5U CN214897420U (en) | 2021-03-27 | 2021-03-27 | Flight instrument liquid crystal display module |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214897420U true CN214897420U (en) | 2021-11-26 |
Family
ID=78871495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120620942.5U Expired - Fee Related CN214897420U (en) | 2021-03-27 | 2021-03-27 | Flight instrument liquid crystal display module |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214897420U (en) |
-
2021
- 2021-03-27 CN CN202120620942.5U patent/CN214897420U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211126 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |