CN214046306U - A connectable and expandable signal analysis module for aerospace - Google Patents
A connectable and expandable signal analysis module for aerospace Download PDFInfo
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- CN214046306U CN214046306U CN202120056710.1U CN202120056710U CN214046306U CN 214046306 U CN214046306 U CN 214046306U CN 202120056710 U CN202120056710 U CN 202120056710U CN 214046306 U CN214046306 U CN 214046306U
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- analysis module
- signal analysis
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 24
- 230000017525 heat dissipation Effects 0.000 claims abstract description 22
- 239000004411 aluminium Substances 0.000 claims description 17
- 238000009434 installation Methods 0.000 claims description 11
- 238000003466 welding Methods 0.000 claims description 2
- 238000012423 maintenance Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 208000021760 high fever Diseases 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
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Abstract
本实用新型公开了一种航天航空用可衔接扩展的信号分析模块，属于航天航空技术领域，所述航天航空用可衔接扩展的信号分析模块包括机箱，所述机箱两侧可拆卸连接有铰链，所述铰链上端可拆卸连接有侧边壳，所述机箱内侧壁固定连接有安装杆，所述安装杆与侧边壳上均开设有螺孔，所述螺孔内部螺纹连接有安装螺丝，所述机箱内部安装有信号分析模块板。本实用新型中信号分析模块板运行所产生的高热通过导热片导入导热条，再经过导热条分布到下方的散热铝鳍片中，散热铝鳍片极大程度上增加有散热面积，配合负压风机接通电源工作鼓风，对散热铝鳍片上的热量进行挥散，通过进风口进风，最终通过散热口将热量排出到外界，适合被广泛推广和使用。
The utility model discloses a connectable and expandable signal analysis module for aerospace, which belongs to the technical field of aerospace. The connectable and expandable signal analysis module for aerospace comprises a chassis, two sides of the chassis are detachably connected with hinges, A side shell is detachably connected to the upper end of the hinge, and a mounting rod is fixedly connected to the inner side wall of the chassis. The mounting rod and the side shell are both provided with screw holes, and the screw holes are threadedly connected with mounting screws. A signal analysis module board is installed inside the chassis. In the utility model, the high heat generated by the operation of the signal analysis module board is introduced into the heat-conducting strips through the heat-conducting strips, and then distributed to the heat-dissipating aluminum fins below through the heat-conducting strips. The heat-dissipating aluminum fins greatly increase the heat-dissipating area. When the fan is connected to the power supply, it works to blow air, and the heat on the heat dissipation aluminum fins is dissipated, and the air is fed through the air inlet, and finally the heat is discharged to the outside through the heat dissipation port, which is suitable for widespread promotion and use.
Description
Technical Field
The utility model relates to an aerospace technical field especially relates to a signal analysis module that can link up extension for aerospace.
Background
Aviation refers to the navigation activity of an aircraft in the earth's atmosphere, and aerospace refers to the navigation activity of an aircraft in the space outside the atmosphere. Aerospace has greatly changed the structure of transportation. Through the rapid development in the last century, aerospace has become the most active and influential scientific and technological field in the 21 st century, and the significant achievement in the field marks the high development of human civilization and also represents an advanced level of national science and technology.
At present, the signal analysis module for aerospace has the following defects: 1. when the internal signal analysis module is overheated or has current faults, the whole case provided with the signal analysis module is inconvenient to disassemble and maintain; 2. the signal analysis module of space flight and aviation needs to operate and calculate huge base information quantity, which easily causes overheating damage. Therefore, a connectible extension signal analysis module for aerospace is provided.
SUMMERY OF THE UTILITY MODEL
The utility model provides a space flight and aviation is with linking up signal analysis module of extension, the produced high fever of signal analysis module board operation passes through the leading-in heat conduction strip of conducting strip, in the heat dissipation aluminium fin of below is distributed to through heat conduction strip again, it has heat radiating area to increase on the very big degree of heat dissipation aluminium fin, cooperation negative pressure fan switch-on power supply work blast air, the heat on the heat dissipation aluminium fin is waved, through the air intake air, finally discharge the heat to the external world through the thermovent, can effectively solve the problem in the background art.
The utility model provides a specific technical scheme as follows:
the utility model provides a pair of aerospace is with linking up signal analysis module of extension, the load simulator comprises a case, machine case both sides can be dismantled and be connected with the hinge, the hinge upper end can be dismantled and be connected with the side shell, machine incasement wall fixedly connected with installation pole, the screw has all been seted up on installation pole and the side shell, the inside threaded connection of screw has the installation screw, machine incasement portion installs signal analysis module board, signal analysis module board skin weld has the conducting strip, the welding of conducting strip lower extreme has the heat conduction strip, heat conduction strip lower extreme fixedly connected with heat dissipation aluminium fin.
Optionally, the outer side wall of the case is provided with a viewing mirror window.
Optionally, the outer side wall of the chassis is provided with an expansion socket.
Optionally, the lower end of the case is fixedly connected with a wheel carrier, and the lower end of the wheel carrier is rotatably connected with a roller.
Optionally, the left side of the case is provided with a heat dissipation port, and the right side of the case is provided with an air inlet.
Optionally, a negative pressure fan is installed on the inner wall of the bottom of the case.
The utility model has the advantages as follows:
1. the utility model discloses it is practical, convenient operation and excellent in use effect, dismantle the installation screw through using relevant instrument, then the side shell is opened under the hinge fit activity of side shell lower extreme, the back is opened to the side shell at quick-witted case both ends, the staff has sufficient space to overhaul the quick-witted incasement portion signal analysis module board and maintain, also can pull down the signal analysis module board and maintain, easy maintenance has solved when the internal signal analysis module appears overheated or current fault, the problem of the maintenance is not convenient for to dismantle by the whole quick-witted case that is equipped with signal analysis module.
2. The utility model discloses in, the produced high fever of signal analysis module board operation passes through the leading-in heat conduction strip of conducting strip, conducting strip and heat conduction strip all adopt aluminium system material to make, the heat conductivity is good and low in cost, in the heat dissipation aluminium fin of below is distributed to through the heat conduction strip again, it has heat radiating area to increase on the heat dissipation aluminium fin very big degree, cooperation negative pressure fan switch-on work air blast, wave the heat on the heat dissipation aluminium fin, through the air intake air inlet, finally discharge the heat to the external world through the thermovent, the signal analysis module of having solved space flight and aviation need the information content of operation calculation huge cardinal number, lead to the problem of overheated damage very easily.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
Fig. 1 is a schematic overall structure diagram of an engageable and expandable signal analysis module for aerospace according to an embodiment of the present invention;
fig. 2 is a schematic cross-sectional view of a chassis of an engageable and expandable signal analysis module for aerospace according to an embodiment of the present invention;
fig. 3 is an assembly schematic diagram of a chassis of an engageable and expandable signal analysis module for aerospace according to an embodiment of the present invention;
in the figure: 1. a chassis; 2. an observation mirror window; 3. an expansion socket; 4. a hinge; 5. mounting screws; 6. mounting a rod; 7. a side shell; 8. a signal analysis module board; 9. a heat conductive sheet; 10. a heat conducting strip; 11. heat dissipating aluminum fins; 12. a heat dissipation port; 13. an air inlet; 14. a negative pressure fan; 15. a wheel carrier; 16. and a roller.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the present invention will be described in further detail with reference to the accompanying drawings, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in 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.
The following will describe in detail a connectable extended signal analysis module for aerospace according to an embodiment of the present invention with reference to fig. 1 to 3.
As shown in fig. 1-3, a signal analysis module for aerospace use capable of linking and expanding comprises a case 1, wherein hinges 4 are detachably connected to two sides of the case 1, side shells 7 are detachably connected to the upper ends of the hinges 4, an installation rod 6 is fixedly connected to the inner side wall of the case 1, screw holes are formed in the installation rod 6 and the side shells 7, installation screws 5 are connected to the screw holes in a threaded manner, a signal analysis module plate 8 is installed inside the case 1, a heat conduction sheet 9 is welded to the outer surface of the signal analysis module plate 8, a heat conduction strip 10 is welded to the lower end of the heat conduction sheet 9, and heat dissipation aluminum fins 11 are fixedly connected to the lower end of the heat conduction strip 10.
In the embodiment, as shown in fig. 1-3, the mounting screws 5 are disassembled by using related tools, then the hinge 4 at the lower end of the side shell 7 is matched with the movable side shell 7 to be opened, after the side shells 7 at the two ends of the chassis 1 are opened, a worker has enough space to overhaul and maintain the signal analysis module board 8 inside the chassis 1, and the signal analysis module board 8 can be disassembled and maintained, so that the maintenance is convenient, and the problem that the whole chassis provided with the signal analysis module is inconvenient to disassemble and maintain when the internal signal analysis module is overheated or has a current fault is solved; the high heat that signal analysis module board 8 operation produced leads to heat conduction strip 10 through conducting strip 9, conducting strip 9 and heat conduction strip 10 all adopt aluminium material to make, the heat conductivity is good and low in cost, in heat dissipation aluminium fin 11 of below distributes through heat conduction strip 10 again, heat dissipation aluminium fin 11 increases to a great extent has heat radiating area, cooperation negative-pressure air fan 14 switch-on power supply work blast air, volatilize the heat on heat dissipation aluminium fin 11, through air intake 13 air inlet, finally discharge the heat to the external world through thermovent 12, the problem that the signal analysis module of space flight and aviation need the operation to calculate huge cardinal number of information volume, lead to overheated damage very easily.
Wherein, the observation mirror window 2 is installed to the chassis 1 lateral wall.
In this embodiment, as shown in fig. 1, the situation can be observed from the inside of the enclosure 1 through the observation mirror window 2.
Wherein, the outer side wall of the case 1 is provided with an expansion socket 3.
In this embodiment, as shown in fig. 1, other equipment pieces can be inserted through the expansion socket 3 for information splicing expansion.
The lower end of the case 1 is fixedly connected with a wheel carrier 15, and the lower end of the wheel carrier 15 is rotatably connected with a roller 16.
In this embodiment, as shown in fig. 1, the wheel frame 15 is connected to the roller 16, and the roller 16 is rotated to move the whole device.
The left side of the case 1 is provided with a heat dissipation port 12, and the right side of the case 1 is provided with an air inlet 13.
In this embodiment, as shown in fig. 2, air is introduced through the air inlet 13, and finally the heat is discharged to the outside through the heat dissipating port 12.
Wherein, the inner wall of the bottom of the case 1 is provided with a negative pressure fan 14.
In this embodiment, as shown in fig. 2, the negative pressure fan 14 is powered on to blow air to dissipate heat from the aluminum fins 11.
It should be noted that the utility model relates to a but space flight and aviation is with linking up expanded signal analysis module, in operation, the staff dismantles installation screw 5 through using relevant instrument, then the hinge 4 cooperation activity side shell 7 of side shell 7 lower extreme is opened down, after the side shell 7 at quick-witted case 1 both ends is opened, the staff has enough space to overhaul and maintain the internal signal analysis module board 8 of quick-witted case 1, also can dismantle the signal analysis module board 8 and maintain, easy maintenance, when the internal signal analysis module appears overheated or current fault, the problem that the whole quick-witted case that is equipped with signal analysis module is not convenient for dismantling the maintenance is solved; the high heat that signal analysis module board 8 operation produced leads to heat conduction strip 10 through conducting strip 9, conducting strip 9 and heat conduction strip 10 all adopt aluminium material to make, the heat conductivity is good and low in cost, in heat dissipation aluminium fin 11 of below distributes through heat conduction strip 10 again, heat dissipation aluminium fin 11 increases to a great extent has heat radiating area, cooperation negative-pressure air fan 14 switch-on power supply work blast air, volatilize the heat on heat dissipation aluminium fin 11, through air intake 13 air inlet, finally discharge the heat to the external world through thermovent 12, the problem that the signal analysis module of space flight and aviation need the operation to calculate huge cardinal number of information volume, lead to overheated damage very easily. The specific model of the component is G-71A negative pressure fan.
The utility model discloses a case 1; an observation mirror window 2; an expansion socket 3; a hinge 4; mounting screws 5; a mounting rod 6; a side case 7; a signal analysis module board 8; a heat conductive sheet 9; a heat conductive strip 10; heat dissipating aluminum fins 11; a heat dissipation port 12; an air inlet 13; a negative pressure fan 14; a wheel frame 15; the roller 16 components are all standard or known to those skilled in the art and their construction and principle are known to those skilled in the art through technical manuals or through routine experimentation.
It is apparent that those skilled in the art can make various changes and modifications to the embodiments of the present invention without departing from the spirit and scope of the embodiments of the present invention. Thus, if such modifications and variations of the embodiments of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (6)
1. The utility model provides a space flight and aviation is with linking up signal analysis module of extension, includes quick-witted case (1), its characterized in that, quick-witted case (1) both sides can be dismantled and be connected with hinge (4), hinge (4) upper end can be dismantled and be connected with side shell (7), quick-witted case (1) inside wall fixedly connected with installation pole (6), the screw has all been seted up on installation pole (6) and side shell (7), screw internal thread is connected with installation screw (5), quick-witted case (1) internally mounted has signal analysis module board (8), signal analysis module board (8) skin weld has conducting strip (9), the welding of conducting strip (9) lower extreme has heat conduction strip (10), heat conduction strip (10) lower extreme fixedly connected with heat dissipation aluminium fin (11).
2. The spaceflight and aviation connectible extension signal analysis module according to claim 1, wherein the outer side wall of the case (1) is provided with a view mirror window (2).
3. The spaceflight and aviation connectable expansion signal analysis module according to claim 1, wherein the outer side wall of the case (1) is provided with an expansion socket (3).
4. The connectible and extendable signal analysis module for aerospace use according to claim 1, wherein a wheel carrier (15) is fixedly connected to the lower end of the case (1), and a roller (16) is rotatably connected to the lower end of the wheel carrier (15).
5. The connectable and expandable signal analysis module for aerospace use according to claim 1, wherein the left side of the case (1) is provided with a heat dissipation port (12), and the right side of the case (1) is provided with an air inlet (13).
6. The spaceflight and aviation connectable extension signal analysis module according to claim 1, wherein a negative pressure fan (14) is mounted on the inner wall of the bottom of the case (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120056710.1U CN214046306U (en) | 2021-01-11 | 2021-01-11 | A connectable and expandable signal analysis module for aerospace |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120056710.1U CN214046306U (en) | 2021-01-11 | 2021-01-11 | A connectable and expandable signal analysis module for aerospace |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214046306U true CN214046306U (en) | 2021-08-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120056710.1U Expired - Fee Related CN214046306U (en) | 2021-01-11 | 2021-01-11 | A connectable and expandable signal analysis module for aerospace |
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| CN (1) | CN214046306U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119342781A (en) * | 2024-10-21 | 2025-01-21 | 航天特种材料及工艺技术研究所 | A lightweight composite chassis with electromagnetic compatibility and high heat dissipation |
-
2021
- 2021-01-11 CN CN202120056710.1U patent/CN214046306U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119342781A (en) * | 2024-10-21 | 2025-01-21 | 航天特种材料及工艺技术研究所 | A lightweight composite chassis with electromagnetic compatibility and high heat dissipation |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210824 |
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| CF01 | Termination of patent right due to non-payment of annual fee |