CN202285098U - Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester - Google Patents
Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester Download PDFInfo
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- CN202285098U CN202285098U CN2011203994186U CN201120399418U CN202285098U CN 202285098 U CN202285098 U CN 202285098U CN 2011203994186 U CN2011203994186 U CN 2011203994186U CN 201120399418 U CN201120399418 U CN 201120399418U CN 202285098 U CN202285098 U CN 202285098U
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- 230000000007 visual effect Effects 0.000 title claims abstract description 15
- 238000005516 engineering process Methods 0.000 title claims abstract description 11
- 238000004891 communication Methods 0.000 claims abstract description 17
- 102100003351 YBX1 Human genes 0.000 claims description 7
- 101700046316 YBX1 Proteins 0.000 claims description 7
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 3
- 230000003247 decreasing Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
Abstract
The utility model discloses an advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester, which comprises an ARM processor unit, external buses to be tested, a bus communication concentrator and a display screen, wherein the external buses to be tested comprise an aeronautical radio incorporated (ARINC) 429 bus, a commercial standard data bus (CSDB) and an RS-422 bus, and are connected with external bus interfaces of the bus communication concentrator respectively; the bus communication concentrator is connected with the ARM processor unit through a personal computer (PC) 104 internal bus; and the display screen is connected with an output terminal of the ARM processor unit. Monitoring tests in the three buses are integrated, so that the monitoring tester is convenient for site technical personnel to use, and monitoring efficiency is improved; the high-performance ARM processor unit is adopted instead of conventional central processing unit (CPU) equipment, so that an equipment volume and energy consumption are reduced, and cost is also decreased; and a visual testing environment is provided, and a user can realize related functions in a testing process through a virtual panel, so that the monitoring tester is visual and convenient to use.
Description
Technical field
The utility model relates to a kind of visual aviation multibus control and measuring appearance based on the ARM technology.
Background technology
In modern times in the Aircraft Design process; Avionics system becomes increasingly complex; The interface multi-communication protocol is varied, and wherein, ARINC429 bus, CSDB bus and RS-422 bus are aircraft general assembly (GA) stage testbus interfaces commonly used; Also being between each system or the predominating path of equipment room digital information transmission, is " nerve " of aircraft.
Yet; Existing aviation monitoring bus proving installation adopts CPU equipment as center processor, and equipment volume is bigger, is not easy to very much the field technician and uses; The energy consumption of CPU equipment is higher simultaneously, cost is also higher, can not adapt to the application and the popularization of aviation monitoring bus proving installation.In addition, traditional aviation monitoring bus proving installation can only be monitored and test single bus, can't monitor multiple bus simultaneously, and the efficient of control and measuring is lower; Visual test environment can't be provided, can't realize control, data acquisition, DATA REASONING and functions such as analysis and The measured results show equipment under test.
The utility model content
The purpose of the utility model is to solve the deficiency of existing aviation monitoring bus proving installation; A kind of novel visual aviation multibus control and measuring appearance based on the ARM technology is provided; Overcoming conventional bus control and measuring equipment adopts CPU equipment as center processor; Equipment volume is bigger, is not easy to the field technician and uses, and the energy consumption of CPU equipment is higher simultaneously, cost is also higher; Can only monitor and test single bus, can't monitor multiple bus simultaneously, the efficient of control and measuring be lower; Visual test environment can't be provided, can't realize shortcoming such as control, data acquisition, DATA REASONING and analysis and The measured results show function equipment under test.
The purpose of the utility model realizes through following technical scheme: a kind of visual aviation multibus control and measuring appearance based on the ARM technology; It comprises arm processor unit, outside bus to be measured, bus communication hub and display screen; Outside bus to be measured comprises ARINC429 bus, CSDB bus and RS-422 bus; Bus outside to be measured is the external bus interface of connecting bus communication hub respectively; Be connected through the PC104 internal bus between bus communication hub and the arm processor unit, display screen is connected with a lead-out terminal of arm processor unit.
The utility model also comprises a keyboard and mouse group, and keyboard is connected with the control terminal of arm processor unit respectively with mouse.
The utility model also comprises a power module, and power module is connected with the power supply terminal of arm processor unit and the power end of bus communication hub respectively.
The beneficial effect of the utility model is:
(1) ARINC429, CSDB and three kinds of monitoring bus tests of RS-422 are integrated, make things convenient for the field technician to use and improved monitoring efficient;
(2) adopt high performance arm processor unit to replace traditional C PU equipment, reduced equipment volume, reduced energy consumption and also reduced cost;
(3) visual test environment is provided, the user can accomplish control, data acquisition, DATA REASONING and functions such as analysis and The measured results show to equipment under test through virtual panel, uses directly perceived more and convenient.
Description of drawings
Fig. 1 is the utility model structural representation block scheme.
Embodiment
The technical scheme of the utility model is described in further detail: as shown in Figure 1 below in conjunction with accompanying drawing; A kind of visual aviation multibus control and measuring appearance based on the ARM technology; It comprises arm processor unit, outside bus to be measured, bus communication hub and display screen; Outside bus to be measured comprises ARINC429 bus, CSDB bus and RS-422 bus; Outside bus to be measured is the external bus interface of connecting bus communication hub respectively, is connected through the PC104 internal bus between bus communication hub and the arm processor unit, and display screen is connected with a lead-out terminal of arm processor unit; It also comprises a keyboard and mouse group and a power module; Keyboard is connected with the control terminal of arm processor unit respectively with mouse; Power module is+5V ,+12V and-12V; Be connected with the power supply terminal of arm processor unit and the power end of bus communication hub respectively, be used for power supply of arm processor unit and the power supply of bus communication relay.
Control and measuring when this monitoring bus tester provides ARINC429, CSDB and three kinds of buses of RS-422, and the detection data that read through the screen on tester output.Powerful graphics environment that the ARM processing unit that carries through instrument provides and function extended capability; Set up patterned virtual panel, the user can accomplish control, data acquisition, DATA REASONING and functions such as analysis and The measured results show to equipment under test through virtual panel.Can under not by the situation of utility appliance and process conditions, accomplish the monitoring analysis to aircraft ARNIC429 bus, CSDB bus and RS-422 bus, bus failure is checked, has improved the accuracy of localization of fault.Adopt up-to-date arm processor unit to replace traditional CPU equipment, reduced equipment volume, the portable field technician of convenience uses; Reduce energy consumption simultaneously and also reduced the tester cost.
Claims (3)
1. visual aviation multibus control and measuring appearance based on ARM technology; It is characterized in that: it comprises arm processor unit, outside bus to be measured, bus communication hub and display screen; Outside bus to be measured comprises ARINC429 bus, CSDB bus and RS-422 bus; Bus outside to be measured is the external bus interface of connecting bus communication hub respectively; Be connected through the PC104 internal bus between bus communication hub and the arm processor unit, display screen is connected with a lead-out terminal of arm processor unit.
2. a kind of visual aviation multibus control and measuring appearance according to claim 1 based on the ARM technology, it is characterized in that: it also comprises a keyboard and mouse group, keyboard is connected with the control terminal of arm processor unit respectively with mouse.
3. a kind of visual aviation multibus control and measuring appearance according to claim 1 based on the ARM technology; It is characterized in that: it also comprises a power module, and power module is connected with the power supply terminal of arm processor unit and the power end of bus communication hub respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203994186U CN202285098U (en) | 2011-10-19 | 2011-10-19 | Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203994186U CN202285098U (en) | 2011-10-19 | 2011-10-19 | Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202285098U true CN202285098U (en) | 2012-06-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011203994186U Expired - Fee Related CN202285098U (en) | 2011-10-19 | 2011-10-19 | Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester |
Country Status (1)
| Country | Link |
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| CN (1) | CN202285098U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103048984A (en) * | 2013-01-17 | 2013-04-17 | 中国民航大学 | Multi-channel ARINC(aeronautical radio incorporated) 700 bus monitoring device and realizing method thereof |
| CN105785833A (en) * | 2014-12-17 | 2016-07-20 | 中车大连电力牵引研发中心有限公司 | Bus analysis apparatus and system for railway vehicles |
| CN113609057A (en) * | 2021-06-28 | 2021-11-05 | 陕西星辰电子技术有限责任公司 | Portable CSDB bus coding and decoding device and method |
-
2011
- 2011-10-19 CN CN2011203994186U patent/CN202285098U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103048984A (en) * | 2013-01-17 | 2013-04-17 | 中国民航大学 | Multi-channel ARINC(aeronautical radio incorporated) 700 bus monitoring device and realizing method thereof |
| CN103048984B (en) * | 2013-01-17 | 2013-12-18 | 中国民航大学 | Multi-channel ARINC(aeronautical radio incorporated) 700 bus monitoring device and realizing method thereof |
| CN105785833A (en) * | 2014-12-17 | 2016-07-20 | 中车大连电力牵引研发中心有限公司 | Bus analysis apparatus and system for railway vehicles |
| CN113609057A (en) * | 2021-06-28 | 2021-11-05 | 陕西星辰电子技术有限责任公司 | Portable CSDB bus coding and decoding device and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 610017 Chengdu hi tech Zone Science and Technology Incubation Park Patentee after: CHENGDU GOLDENWAY TECHNOLOGY CO., LTD. Address before: 610017 Chengdu hi tech Zone Science and Technology Incubation Park Patentee before: Chengdu Goldenway Technology Co.,Ltd. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester Effective date of registration: 20131204 Granted publication date: 20120627 Pledgee: Xi'an hi tech Development Zone Guoxin micro credit Co., Ltd. Pledgor: CHENGDU GOLDENWAY TECHNOLOGY CO., LTD. Registration number: 2013990000924 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Advanced RISC machine (ARM)-technology-based visual aeronautical multi-bus monitoring tester Effective date of registration: 20131204 Granted publication date: 20120627 Pledgee: Xi'an hi tech Development Zone Guoxin micro credit Co., Ltd. Pledgor: CHENGDU GOLDENWAY TECHNOLOGY CO., LTD. Registration number: 2013990000924 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20141229 Granted publication date: 20120627 Pledgee: Xi'an hi tech Development Zone Guoxin micro credit Co., Ltd. Pledgor: CHENGDU GOLDENWAY TECHNOLOGY CO., LTD. Registration number: 2013990000924 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20161129 Address after: 610041 Chengdu hi tech Zone Science and Technology Incubation Park Patentee after: Chengdu Goldenway Electronic Co., Ltd. Address before: 610017 Chengdu hi tech Zone Science and Technology Incubation Park Patentee before: CHENGDU GOLDENWAY TECHNOLOGY CO., LTD. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120627 Termination date: 20171019 |