CN203658905U - Server for processing data in airborne information system network - Google Patents
Server for processing data in airborne information system network Download PDFInfo
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- CN203658905U CN203658905U CN201320740962.1U CN201320740962U CN203658905U CN 203658905 U CN203658905 U CN 203658905U CN 201320740962 U CN201320740962 U CN 201320740962U CN 203658905 U CN203658905 U CN 203658905U
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- server
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- power source
- data
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- 238000012360 testing method Methods 0.000 description 2
- KKIMDKMETPPURN-UHFFFAOYSA-N 1-(3-(trifluoromethyl)phenyl)piperazine Chemical compound FC(F)(F)C1=CC=CC(N2CCNCC2)=C1 KKIMDKMETPPURN-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
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- 101000919360 Homo sapiens Cytochrome P450 2C18 Proteins 0.000 description 1
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- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
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- 238000001514 detection method Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
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Abstract
The utility model provides a server for processing data in an airborne information system network. The server comprises a casing, an interface group, a processor, an aircraft power source module, a temperature sensor, a storage, an internal storage, a clock timer and a network switch, wherein the interface group is embedded in the casing, the processor is arranged in the casing, and the aircraft power source module, the temperature sensor, the storage, the internal storage, the clock timer and the network switch are connected with the processor. A power source monitoring module is connected between the aircraft power source module and the processor, an alternating current indication lamp, a direct current indication lamp and a self-inspection indication lamp are arranged on the casing, the alternating current indication lamp and the direct current indication lamp are connected with the power source monitoring module, and the self-inspection indication lamp is connected with the processor. The server for processing data in the airborne information system network has functions of safety, reliability, built-in self inspection and the like.
Description
Technical field
The utility model relates to a kind of server, relates in particular to a kind of server for the treatment of data in airborne information systems internetting.
Background technology
On-board server is the special purpose computer for the treatment of airborne infosystem specific transactions, by residing in the application software in this equipment, for airborne infosystem provides various application services, as print service, integrated maintenance service, aircraft parameter services etc., crew uses these services by main cabin core system and driving cabin information subsystem.
The webserver possesses large capacity storage capability and high-performance calculation ability, the data that support meets ARINC 615A-3 specification load agreement, the resident running environment of application software (comprising third party's application software) of infosystem is provided, and the function of data storage, forwarding and management etc.
Utility model content
The technical matters that the utility model mainly solves is to provide a kind of server for the treatment of data in airborne information systems internetting, has the functions such as security, reliability and built in test.
For solving the problems of the technologies described above, the technical scheme that the utility model adopts is: a kind of server for the treatment of data in airborne information systems internetting is provided, comprise housing, be embedded at the interface group on housing, be located at the processor in housing, the airplane power source module being connected with described processor respectively, temperature sensor, storer, internal memory, clock timer, the network switch, between described airplane power source module and described processor, be connected with Power Monitoring Unit, on described housing, be also provided with the AC power pilot lamp being connected with described Power Monitoring Unit, direct supply pilot lamp and the self-inspection pilot lamp being connected with described processor.
Wherein, described interface group comprises airplane power source interface, debugging interface and gigabit network interface, and described airplane power source interface is connected with described airplane power source module, and described debugging interface is connected with described processor.
Wherein, described debugging interface comprises 1 road RS232 debug serial port and 1 road 100Mbps debugging serial interface.
Wherein, described airplane power source module is the airplane power source modular converter that 115V AC power is converted to 12V direct supply.
Wherein, described storer comprises the solid state hard disc of Flash flash memory and SATA interface.
Wherein, described gigabit network interface comprises the 1000Mbps network interface that 10 tunnels are connected with the described network switch.
Wherein, the described network switch is three-tier switch.
The beneficial effects of the utility model are: the situation that is different from prior art, server for the treatment of data in airborne information systems internetting of the present utility model can make described server have higher safety and reliability and built in test function, also be provided with multiple pilot lamp so that user can understand the operation conditions of server easily, book server functional diversities, is user-friendly to.
Brief description of the drawings
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skill in the art, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the block scheme of the utility model for the treatment of the server of data in airborne information systems internetting.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtaining under creative work prerequisite, all belong to the scope of the utility model protection.
The housing for the treatment of the server of data in airborne information systems internetting of the present embodiment, cabinet adopts aluminium alloy, and the color of described cabinet adopts ink black, corresponding colour atla RAL9005, structure meets ARINC600 specification.Described server is of a size of 2MCU, has and meets electromagnetic screen and the grounding design that ARINC600 specifies.The inside of server adopts the CPCI back of the body to plug meter, makes cabinet inside without cable, more convenient assembly and disassembly, and outside employing air blast cooling, pressure drop meets ARINC600 specification.Case front panel is provided with handle, does not have sharp edge, and edge is through overprotection or round and smooth processing.The front panel of cabinet provides 3 pilot lamp, i.e. the normal pilot lamp of 115V AC power, the normal pilot lamp of inner direct supply and self-inspection pilot lamp.The normal pilot lamp of described 115V AC power normally indicates class to be all connected with described Power Monitoring Unit with described inner direct supply, is and shows output when normal for monitor described AC power and direct supply when Power Monitoring Unit; Described self-inspection pilot lamp is connected with described processor, for detecting that when processor equipment shows output while normally work.
The data of the webserver load and meet ARINC615A-3 protocol specification, carry out data loading by self or PMAT from ethernet communication interface, can upgrade by the mode application programs and the configuration file that load, when data load unsuccessfully, the webserver is by the normal operating conditions returning to before loading, no matter load successfully or failure, all will generate loading daily record, and be stored in this locality.The webserver is stored self configuration information and (is comprised current device supplier information in configuration file, equipment piece number information, software version etc.), support to check network connection, network traffics and network configuration information by Web interface, by SNMP(Simple Network Management Protocol, Simple Network Management Protocol) agreement obtains network connection, network traffics and the network configuration information of self.The webserver in the present embodiment has device identification, can prevent from obscuring with other equipment, and external interface has Anti-misplug design, and webserver reply external interface provides ESD(Electro-Static Discharge, and static discharges) protection.The webserver has internal protection circuitry design, ensures the security of equipment in reversal connection situation, and in the time that external ac power source keeps power supply, the webserver can be taken away or replace, and self and other equipment is not caused to damage.
Particularly, refer to Fig. 1, Fig. 1 is the block scheme of the utility model for the treatment of the server of data in airborne information systems internetting.The described server for the treatment of data in airborne information systems internetting comprises housing 100, be embedded at interface group on housing 100, be located at processor 102 in housing 100, be connected with described processor 102 respectively airplane power source module 104, temperature sensor 105, storer 106, internal memory 107, clock timer 108, the network switch 109 are connected with Power Monitoring Unit 110 between described airplane power source module 104 and described processor 102.Wherein:
Described housing 100 is the cabinet of 2MCU model, and housing 100 is provided with interface group and pilot lamp, is also provided with reset key.
Described interface group comprises airplane power source interface 1011, debugging interface 1012 and gigabit network interface 1013.
Table 1
Refer to table 1, described airplane power source interface 1011 is connected with described airplane power source module 104, for the 115V AC power on aircraft is linked into airplane power source module 104.
Described debugging interface 1012 comprises 1 road RS232 debug serial port and 1 road 100Mbps debugging serial interface.Described RS232 debug serial port is connected with described processor 102, for the debugging of serial port terminal; Described 100Mbps debugging serial interface is connected with described processor 102, for access means Web interface, and TFTP transmission etc.
Described gigabit network interface 1013 is the 1000Mbps network interface being connected with described switch, is connected 10 road 1000Mbps network interface for accessing other equipment in avionics system with switch.
Described airplane power source module 104 is a power transfer module, it is connected with described processor 102 by Power Monitoring Unit 110, it,, for 115V AC power being converted to by described airplane power source interface 1011 to the direct supply of 12V, thinks that described server provides power supply.In other embodiment, this airplane power source module 104 can also be power module independently, and for example it can be lithium battery, in the time that described independently power module is lithium battery, is also provided with the charging inlet that is used to this lithium cell charging on described server.
Described Power Monitoring Unit 110 is connected between described airplane power source module 104 and described processor 102, and it is monitored for the AC power to airplane power source module 104 and direct supply.Described Power Monitoring Unit 110 can be A.C. voltmeter, D.C. voltmeter, reometer etc., can be also a sensor for sensing voltage, electric current.In the present embodiment, described housing 100 is provided with AC power pilot lamp 111 and direct supply pilot lamp 112, described AC power pilot lamp 111 is connected with described Power Monitoring Unit 110 with direct supply pilot lamp 112, for monitoring AC power, direct supply when described Power Monitoring Unit 110 when normal, show output.
Described temperature sensor 105 is connected with described processor 102, for detection of the running temperature of described secure router inside, and the temperature signal detecting is sent to described processor 102, described processor 102 according to the temperature signal receiving to judge the whether temperature value in normal range of this temperature, if in the temperature value of normal range, do not carry out any processing, if when the temperature value of this temperature in improper scope, processor 102 carries out derate processing.In the present embodiment, described normal temperature value scope is at-15 DEG C～+ 70 DEG C, the temperature value detecting when described temperature sensor 105 is not in above-mentioned scope, and processor 102 carries out derate processing, reaches normal range value with the temperature value that makes described secure router inside.
Described storer 106 comprises Flash flash memory and solid state hard disc, described solid state hard disc adopts 500G big capacity hard disk, so that store more data, described Flash flash memory is compared with traditional memory device, and that described Flash flash memory has is lightweight, volume is little, can repeat erasable number of times high.Book server is established two storeies 106 and has not only been met the requirement of employing hard-disc storage Large Volume Data but also met the requirement that adopts Flash flash memory to be convenient to dismounting, to be convenient for carrying.
Described internal memory 107 adopts the internal storage of the magnesium light board of 2G.In different embodiment, the model of described internal memory 107, large I appropriately adjust.
Described clock timer 108, for processor 102 major clock of working is provided, has high stability, temperature compensation, the feature of low drift.
Described processor 102 is PowerPC processor 102, the data that described processor 102 sends for receiving above-mentioned all parts, and carry out different processing and the packet of needs transmission is carried out to safe handling according to the data of different module transmissions, then by network layer switch, Packet Generation is gone out.In the present embodiment, be also provided with a self-inspection pilot lamp 113 being connected with described processor 102 on housing 100, described self-inspection pilot lamp 113 for showing output in the time that startup of server carries out self-inspection.
In the present embodiment, the described network switch 109 is three-tier switch, described three-tier switch is the switch with part router feature, the most important object of three-tier switch is to accelerate the exchanges data of large-scale LAN (Local Area Network) inside, the routing function having is also this object service, can accomplish route one time, repeatedly forward.Process for regularity such as package forwards is realized by High-Speed Hardware, and the function such as picture updating route information, routing table maintenance, route are calculated, route is determined is realized by software.Three layer-switching technologies are exactly two layer-switching technologies+tri-layer retransmission technique.Tradition switching technology is the OSI network standard model second layer---data link layer operates, and being in network model the 3rd layers, three layer-switching technologies realize the high speed forward of packet, both can realize network routing function, can accomplish optimal network performance according to heterogeneous networks situation again.Described three-tier switch, for receiving the packet that described processor 102 sends, is gone out Packet Generation.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all within spirit of the present utility model and principle, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (7)
1. the server for the treatment of data in airborne information systems internetting, it is characterized in that: comprise housing, be embedded at the interface group on housing, be located at the processor in housing, the airplane power source module being connected with described processor respectively, temperature sensor, storer, internal memory, clock timer, the network switch, between described airplane power source module and described processor, be connected with Power Monitoring Unit, on described housing, be also provided with the AC power pilot lamp being connected with described Power Monitoring Unit, direct supply pilot lamp and the self-inspection pilot lamp being connected with described processor.
2. the server for the treatment of data in airborne information systems internetting as claimed in claim 1, it is characterized in that: described interface group comprises airplane power source interface, debugging interface and gigabit network interface, described airplane power source interface is connected with described airplane power source module, and described debugging interface is connected with described processor.
3. the server for the treatment of data in airborne information systems internetting as claimed in claim 2, is characterized in that: described debugging interface comprises 1 road RS232 debug serial port and 1 road 100Mbps debugging serial interface.
4. the server for the treatment of data in airborne information systems internetting as claimed in claim 1, is characterized in that: described airplane power source module is the airplane power source modular converter that 115V AC power is converted to 12V direct supply.
5. the server for the treatment of data in airborne information systems internetting as claimed in claim 1, is characterized in that: described storer comprises the solid state hard disc of Flash flash memory and SATA interface.
6. the server for the treatment of data in airborne information systems internetting as claimed in claim 2, is characterized in that: described gigabit network interface comprises the 1000Mbps network interface that 10 tunnels are connected with the described network switch.
7. the server for the treatment of data in airborne information systems internetting as claimed in claim 1, is characterized in that: the described network switch is three-tier switch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320740962.1U CN203658905U (en) | 2013-11-20 | 2013-11-20 | Server for processing data in airborne information system network |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320740962.1U CN203658905U (en) | 2013-11-20 | 2013-11-20 | Server for processing data in airborne information system network |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203658905U true CN203658905U (en) | 2014-06-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320740962.1U Expired - Lifetime CN203658905U (en) | 2013-11-20 | 2013-11-20 | Server for processing data in airborne information system network |
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| Country | Link |
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| CN (1) | CN203658905U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113295207A (en) * | 2021-05-14 | 2021-08-24 | 国网江苏省电力有限公司苏州供电分公司 | Power terminal server capable of performing self-checking and use method thereof |
-
2013
- 2013-11-20 CN CN201320740962.1U patent/CN203658905U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113295207A (en) * | 2021-05-14 | 2021-08-24 | 国网江苏省电力有限公司苏州供电分公司 | Power terminal server capable of performing self-checking and use method thereof |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140618 |