CN202904470U - Airborne reinforced integrate computer - Google Patents
Airborne reinforced integrate computer Download PDFInfo
- Publication number
- CN202904470U CN202904470U CN 201220493001 CN201220493001U CN202904470U CN 202904470 U CN202904470 U CN 202904470U CN 201220493001 CN201220493001 CN 201220493001 CN 201220493001 U CN201220493001 U CN 201220493001U CN 202904470 U CN202904470 U CN 202904470U
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Abstract
The utility model provides an airborne reinforced integrate computer which comprises a liquid crystal display module arranged on the front end face of a computer case, a core module arranged inside the computer case, a user module and a heat dissipation module, wherein the core module comprises a main control module and a switch module, the main control module is arranged on the lower portion of the interior of the computer case, the switch module is arranged above the main control module, and the user module is fixedly installed above the core module. Parts in the airborne reinforced integrate computer and interfaces are in a modular structure in an integrated mode, rapid disassembly and assembly can be achieved, meanwhile, all modules all can be independently disassembled and assembled, and maintainability of the airborne reinforced integrate computer is improved.
Description
Technical field
The utility model relates to a kind of airborne reinforcing Integral computer.
Background technology
For can be in aircraft steady operation, simultaneously not can with the mutual interference of miscellaneous equipment generation phase, the computer system of working in airborne circumstance need to have the reinforcement performances such as very strong high-low temperature resistant and anti-vibrating and impact, and will carry out good electromagnetic Compatibility Design.In addition, operating performance, maintainability and the weight of equipment there is strict requirement.
In the ruggedized computer field, the reinforcement performance of airborne equipment and the electric property of equipment, weight, cost and maintainable mutually restriction are serious, particularly along with the advancing by leaps and bounds of computing power index and expanded function, traditional mode is difficult at lower cost and satisfies in the situation that the strict weight of equipment requires adapt to the upgrading requirement.Therefore, research and develop that a kind of reinforcement performance is reliable, powerful, easy to maintenance, excellent in heat dissipation effect, airborne reinforcing all-in-one platform lightweight, that cost is moderate, versatility is good have important practical significance expanded function flexibly.
The utility model content
The technical problems to be solved in the utility model, be exactly for the existing deficiency of prior art, and a kind of airborne reinforcing Integral computer is provided, it adopts modular construction, it is strong to protect malleability, easy accessibility, easy to maintenance, lightweight, cost is moderate, the fast lifting that can adapt to computing power can be worked under abominable airborne circumstance condition, thereby be had very large practical application request.
This programme is achieved by the following technical measures: this airborne reinforcing Integral computer comprises the liquid crystal display device module that is positioned at the cabinet front end face and nucleus module, line module and the radiating module that is positioned at cabinet inside, described nucleus module comprises main control module and switch module, wherein, main control module is positioned at the below of cabinet inside, switch module is positioned at the top of main control module, and line module is fixedly installed in the top of nucleus module.
Above-mentioned main control module comprises from top to bottom successively parallel interior mainboard, electric board module, reservation 6U extension bits and the power module of framework that is fixed on nucleus module.
The rear end face of the framework of above-mentioned nucleus module is provided with mainboard, electric board module, reserves 6U3 groove backboard corresponding to 6U extension bits, also has the power supply backplane corresponding with power module.
The front end face of above-mentioned switch module is provided with the switch tension disc, rear end face is provided with switch backplane, and the rear end face of switch backplane and 6U3 groove backboard has the rear wiring board of grafting in parallel.
State air intake module and reservation air-out module that radiating module comprises complete machine air-out fan and is plugged on respectively the nucleus module both sides.
The intersection of main control module and switch module is provided with the boundary buttress brace on the rear end face of above-mentioned cabinet, leaves the space that leaks out between main control module and the switch module, and this space that leaks out is concordant with the boundary buttress brace.
Above-mentioned cabinet is that aluminium alloy and stainless steel welding form; The rear panel of cabinet is divided into up and down two parts, and upper rear panel is corresponding with the switch module position, and is provided with complete machine air-out fan and interface area on it, and lower rear panel is corresponding with the main control module position, mounting related components not on it.
The device interval layout that the device that above-mentioned nucleus module internal heat generation amount is large and thermal value are little, and between mainboard and the electric board module, electric board module and reserve between the 6U extension bits and reserve between 6U extension bits and the power module and leave the air channel that leaks out.
Above-mentioned liquid crystal display device module comprises front plate, LCDs, shield glass, touch-screen and the front panel that is arranged in order from inside to outside, front plate and cabinet are fixed as one, LCDs is inlaid in the front plate by vibroshock, shield glass covers the LCDs outside, touch-screen covers the shield glass outside, and touch-screen is close to the front panel inboard and compresses shield glass.
Above-mentioned line module is fixedly connected with nucleus module by the module fixing rack of its below, and the two ends of module fixing rack are fixedly connected with the crossbeam of cabinet both sides respectively; Switch module is fixedly connected with the framework of nucleus module by the 6U supporting plate.This version has strengthened resistance to overturning and the reliability of all components and parts of cabinet inside.
The beneficial effect of this programme can be learnt according to the narration to such scheme, (1) be modular construction with the parts in the complete machine and Interface integration, can realize fast assembling-disassembling on the one hand, can finish dismounting or the assembling of complete machine in three minutes, simultaneously, all modules are separately dismounting all, so, its maintainable raising.(2) cabinet adopts aluminium alloy and stainless steel to be welded into, and greatly reduces the weight of complete machine, and the weight of complete machine is maintained below 18 kilograms.(3) arrangement form and the space that leaks out of device in the space that leaks out between main control module and the switch module, the nucleus module, and the form that is arranged in parallel of device in being arranged in parallel of main control module and switch module, main control module, also has in addition radiating module, these radiator structures are convenient to flowing of the interior heat of module, heat in the nucleus module can in time be discharged, the heat that radiating module can distribute the cabinet inside device is rapidly taken away, and can guarantee that the run-in index heat dissipation wind channel of each module is evenly reliable.(4) by adopting switch backplane and the parallel grafting of 6U3 groove backboard with rear wiring board, reduced a large amount of aerial lugs, for the lifting of whole aircraft reliability, maintainability and operating performance provides further assurance.This shows that the utility model compared with prior art has substantive distinguishing features and progress, the beneficial effect of its enforcement also is apparent.
Description of drawings
Fig. 1 is the perspective view one of the utility model embodiment.
Fig. 2 is the perspective view two of the utility model embodiment.
Fig. 3 is the perspective view three of the utility model embodiment.
Fig. 4 is the backsight perspective structure synoptic diagram of the utility model embodiment.
Fig. 5 is the partial schematic sectional view of overlooking of the utility model embodiment.
Fig. 6 is the structural representation of nucleus module.
Fig. 7 is the structural representation of liquid crystal display device module.
Among the figure, 1 is cabinet, and 2 is the air intake module, and 3 is line module, 4 is nucleus module, and 5 is complete machine air-out fan, and 6 are the air-out waveguide, 7 is liquid crystal display device module, and 8 is the air intake waveguide, and 9 is lower rear panel, 10 is interface area, and 11 is upper rear panel, and 12 for reserving the air-out module, 13 are the boundary buttress brace, and 14 is wave filter, and 15 is the switch tension disc, 16 is switch module, and 17 are the space that leaks out, and 18 for reserving the 6U extension bits, 19 is the electric board module, and 20 is power module, and 21 is mainboard, 22 is top cover, and 23 is module fixing rack, and 24 is reinforcement, 25 is switch backplane, and 26 is backboard on the nucleus module, and 27 is backboard under the nucleus module, 28 is power supply backplane, and 29 is rear wiring board, and 30 is 6U3 groove backboard, 31 is front plate, and 32 is front panel, and 33 is shield glass, 34 is touch-screen, and 35 is LCDs, and 36 is the framework of nucleus module.
Embodiment
For clearly demonstrating the technical characterstic of this programme, below by embodiment, and in conjunction with its accompanying drawing, this programme is set forth.
A kind of airborne reinforcing Integral computer, as shown in the figure, it comprises the liquid crystal display device module 7 that is positioned at cabinet 1 front end face and nucleus module 4, line module 3 and the radiating module that is positioned at cabinet 1 inside, described nucleus module 4 comprises main control module and switch module 16, wherein, main control module is positioned at the below of cabinet 1 inside, and switch module 16 is positioned at the top of main control module, and line module 3 is fixedly installed in the top of nucleus module 4.
Wherein, main control module comprises from top to bottom mainboard 21, electric board module 19 in the parallel framework 36 that is fixed on nucleus module successively, reserves 6U extension bits 18 and power module 20.The rear end face of the framework 36 of nucleus module is provided with mainboard 21, electric board module 19, reserves 6U3 groove backboard 30 corresponding to 6U extension bits 18, also has a 6U CPCI power supply backplane 28 corresponding with power module 20.This machine is the cpci bus form, and mainboard 21 connects by the very high pin hole connector of reliability, and the exclusive guideway bar of framework 36 both sides by nucleus module is fixed; Power supply has been selected the very high modular power source of reliability, hard disk has adopted the strong electric board module 19 of vibration resistance, and electric board module 19 wireless dockings are fixed on the 6U CPCI hard disk fixed head, and these devices all have extreme high reliability, and have carried out the suspension isolation processing.
The front end face of switch module 16 is provided with switch tension disc 15, rear end face is provided with switch backplane 25, the rear end face of switch backplane 25 and 6U3 groove backboard 30 has the rear wiring board 29 of grafting in parallel, has realized communicating by letter between switch module 16 and the main control module by rear wiring board 29.In this version, the line of switch module 16 with front and back panel so both shortened in the position above switch module 16 is in nucleus module 4, can plug from cabinet 1 rear side again.
Radiating module comprises complete machine air-out fan 5 and is plugged on respectively the air intake module 2 of nucleus module 4 both sides and reserves air-out module 12.When cabinet 1 internal heat generation amount is large, reserves air-out module 12 and can assist complete machine air-out fan 5 that heat is discharged fast.The intersection of main control module and switch module 16 is provided with boundary buttress brace 13 on the rear end face of cabinet 1, leave the space 17 that leaks out between main control module and the switch module 16, this space 17 that leaks out is concordant with boundary buttress brace 13, in addition, the device interval layout that the device that nucleus module 4 internal heat generation amounts are large and thermal value are little, and between mainboard 21 and the electric board module 19, electric board module 19 and reserve between the 6U extension bits 18 and reserve between 6U extension bits 18 and the power module 20 and leave the air channel that leaks out.This air channel that leaks out cooperates the space 17 that leaks out between main control module and the switch module 16, and the version of the little device interval layout of the large device of thermal value and thermal value, have again, the form that is arranged in parallel of nucleus module 4 interior devices, all these structures, all be beneficial to heat flowing in nucleus module 4, realized the integrated heat dissipation of nucleus module 4, the heat that complete machine air-out fan 5 and reservation air-out module 12 can be distributed nucleus module 4 internal components is rapidly taken away, and has guaranteed that the run-in index heat dissipation wind channel of each module is evenly reliable.
Liquid crystal display device module 7 comprises front plate 31, LCDs 35, shield glass 33, touch-screen 34 and the front panel 32 that is arranged in order from inside to outside, front plate 31 is fixed as one with cabinet 1, LCDs 35 is inlaid in the front plate 31 by vibroshock, shield glass 33 covers LCDs 35 outsides, touch-screen 34 covers shield glass 33 outsides, and touch-screen 34 is close to front panel 32 inboards and compresses shield glass 33.Wherein, LCDs 35 adopts the technical grade screen of high reliability, and it has extreme high reliability, and has carried out the suspension isolation processing.
In addition, power supply, the signal of the 14 pairs of equipment of wave filter by being fixed in upper rear panel 11 places carries out filtering to be processed, and air intake module 2 places are provided with air intake guided wave 8, and complete machine air-out fan 5 places are provided with air-out waveguide 6, and the device interior cable adopts shielded cable; The aluminium alloy that adopts in the cabinet 1 is the aluminum alloy materials that conducts electricity very well; The shielding materials such as conducting foam, aluminium foil and conductive rubber strip are adopted in seam and junction; The shield glass 33 that adopts in the liquid crystal display device module 7, the use of these shielding materials makes complete machine have good capability of electromagnetic shielding.
During dismounting, by front panel 32 places dismounting liquid crystal display device module 7, by top cover 22 places dismounting radiating module and the line module 3 of cabinet 1, by the upper rear panel 11 places dismounting switch module 16 of cabinet 1, by the lower rear panel 9 places dismounting main control module of cabinet 1.Also can be by top cover 22 place's integral disassembly, assembly nucleus modules 4 of cabinet 1.
Can pass through existing techniques in realizing without the technical characterictic of describing in the utility model, not repeat them here.
Claims (10)
1. airborne reinforcing Integral computer, it is characterized in that: it comprises the liquid crystal display device module that is positioned at the cabinet front end face and nucleus module, line module and the radiating module that is positioned at cabinet inside, described nucleus module comprises main control module and switch module, wherein, main control module is positioned at the below of cabinet inside, switch module is positioned at the top of main control module, and line module is fixedly installed in the top of nucleus module.
2. airborne reinforcing Integral computer according to claim 1 is characterized in that: described main control module comprises from top to bottom mainboard, electric board module in the parallel framework that is fixed on nucleus module successively, reserves 6U extension bits and power module.
3. airborne reinforcing Integral computer according to claim 2, it is characterized in that: the rear end face of the framework of described nucleus module is provided with mainboard, electric board module, reserves 6U3 groove backboard corresponding to 6U extension bits, also has the power supply backplane corresponding with power module.
4. airborne reinforcing Integral computer according to claim 3, it is characterized in that: the front end face of described switch module is provided with the switch tension disc, rear end face is provided with switch backplane, and the rear end face of switch backplane and 6U3 groove backboard has the rear wiring board of grafting in parallel.
5. airborne reinforcing Integral computer according to claim 1 is characterized in that: described radiating module comprises complete machine air-out fan and is plugged on respectively the air intake module of nucleus module both sides and reserves the air-out module.
6. airborne reinforcing Integral computer according to claim 5, it is characterized in that: the intersection of main control module and switch module is provided with the boundary buttress brace on the rear end face of described cabinet, leave the space that leaks out between main control module and the switch module, this space that leaks out is concordant with the boundary buttress brace.
7. airborne reinforcing Integral computer according to claim 1 is characterized in that: described cabinet is that aluminium alloy and stainless steel welding form; The rear panel of cabinet is divided into up and down two parts, and upper rear panel is corresponding with the switch module position, and is provided with complete machine air-out fan and interface area on it, and lower rear panel is corresponding with the main control module position, mounting related components not on it.
8. airborne reinforcing Integral computer according to claim 3, it is characterized in that: the device interval layout that the device that described nucleus module internal heat generation amount is large and thermal value are little, and between mainboard and the electric board module, electric board module and reserve between the 6U extension bits and reserve between 6U extension bits and the power module and leave the air channel that leaks out.
9. according to claim 1,2,3 or 4 described airborne reinforcing Integral computers, it is characterized in that: described liquid crystal display device module comprises front plate, LCDs, shield glass, touch-screen and the front panel that is arranged in order from inside to outside, front plate and cabinet are fixed as one, LCDs is inlaid in the front plate by vibroshock, shield glass covers the LCDs outside, touch-screen covers the shield glass outside, and touch-screen is close to the front panel inboard and compresses shield glass.
10. according to claim 1,2,3 or 4 described airborne reinforcing Integral computers, it is characterized in that: described line module is fixedly connected with nucleus module by the module fixing rack of its below, and the two ends of module fixing rack are fixedly connected with the crossbeam of cabinet both sides respectively; Switch module is fixedly connected with the framework of nucleus module by the 6U supporting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220493001 CN202904470U (en) | 2012-09-26 | 2012-09-26 | Airborne reinforced integrate computer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220493001 CN202904470U (en) | 2012-09-26 | 2012-09-26 | Airborne reinforced integrate computer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202904470U true CN202904470U (en) | 2013-04-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220493001 Expired - Fee Related CN202904470U (en) | 2012-09-26 | 2012-09-26 | Airborne reinforced integrate computer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202904470U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102880247A (en) * | 2012-09-26 | 2013-01-16 | 济南腾越电子有限公司 | Airborne reinforcement integrating computer |
| CN108169593A (en) * | 2017-12-18 | 2018-06-15 | 西安翌飞核能装备股份有限公司 | A kind of modularization, the instrument that assembled inside is carried out using guide rail |
-
2012
- 2012-09-26 CN CN 201220493001 patent/CN202904470U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102880247A (en) * | 2012-09-26 | 2013-01-16 | 济南腾越电子有限公司 | Airborne reinforcement integrating computer |
| CN102880247B (en) * | 2012-09-26 | 2014-12-03 | 济南腾越电子有限公司 | Airborne reinforcement integrating computer |
| CN108169593A (en) * | 2017-12-18 | 2018-06-15 | 西安翌飞核能装备股份有限公司 | A kind of modularization, the instrument that assembled inside is carried out using guide rail |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130424 Termination date: 20150926 |
|
| EXPY | Termination of patent right or utility model |