CN203299611U - Aviation integrated-data acquisition and control system - Google Patents
Aviation integrated-data acquisition and control system Download PDFInfo
- Publication number
- CN203299611U CN203299611U CN2013202338333U CN201320233833U CN203299611U CN 203299611 U CN203299611 U CN 203299611U CN 2013202338333 U CN2013202338333 U CN 2013202338333U CN 201320233833 U CN201320233833 U CN 201320233833U CN 203299611 U CN203299611 U CN 203299611U
- Authority
- CN
- China
- Prior art keywords
- board
- bus interface
- interface
- control system
- collection
- 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 - Lifetime
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
Abstract
The utility model discloses an aviation integrated-data acquisition and control system. The system includes a power board, a backboard and an interface board. The power board is connected with a data control and processing board, a digital-signal acquisition board, a first analog-signal acquisition board, a second analog-signal acquisition board and an indication board respectively. All of the data control and processing board, the digital-signal acquisition board, the first analog-signal acquisition board and the second analog-signal acquisition board are connected to the backboard through CPCI buses. An output end of the data control and processing board is connected to an input end of the indication board. All of the data control and processing board, the digital-signal acquisition board, the first analog-signal acquisition board and the second analog-signal acquisition board are connected to the interface board. The system is capable of acquiring a plurality of kinds of signals and integrating a cache record card in an acquisition device so that rapid and highly efficient data maintenance and management are realized on the acquisition machine and instantaneity and concurrent ability are higher. The aviation integrated-data acquisition and control system can be widely applied to the field of avionic devices as an aviation integrated-data acquisition and control system.
Description
Technical field
The utility model relates to the avionic device field, and especially a kind of aviation integrated data gathers and control system.
Background technology
Explanation of nouns:
GJB289A: military standard, digital time-devision system/response type multiplex data bus;
ARINC429: digital information transmission system DITS(digital information transmission system);
HUMS: helicopter health is a complication system that integrates avionic device, ground-support equipment and airborne computer monitoring diagnostic product with usage monitoring system (HUMS).
Along with the development of aeronautical technology, the needs collection on aircraft and the signal kinds of record are more and more, data volume is increasing, and collection and the registering capacity of existing Flight Data Record System for Aircraft can not satisfy the demands.
Existing Flight Data Record System for Aircraft, due to the restriction that is subject to hardware resource, gathers kind less, can not gather AFDX and Ethernet data, and the capacity of record and registering capacity can not satisfy the demands.Existing flight parameter acquisition system is all the more limited hardware platform of resourceoriented, high-performance embedded hardware platform for many calculating and storage capacity, real-time and the higher system of concurrent ability need to be arranged, give full play to the performance of hardware, realize synchronous acquisition, reception, processing and the memory function of multiple types, high data volume data.
The utility model content
In order to solve the problems of the technologies described above, the purpose of this utility model is: provide a kind of can gather simultaneously multi-signal, be convenient to safeguard have the more collection of aviation integrated data and a control system of high real-time and concurrent ability.
The technical scheme that the utility model adopts is: a kind of aviation integrated data gathers and control system, this system includes power panel, backboard and interface board, and described power panel is connected with respectively Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate, the second collection of simulant signal plate and indicator board; Described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to backboard by cpci bus, the output terminal of described Data Control disposable plates is connected to the input end of indicator board, and described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to interface board.
Further, described Data Control disposable plates is connected with the fast recording card by the SATA bus.
Further, described fast recording card adopts reinforcement type FLASH hard disk.
Further, described power panel includes normal power source input end and emergency power pack input end, and described power panel includes at least three DC voltage output ends for the internal system power supply.
Further, described interface board is provided with GJB289A bus interface, industry ethernet interface and RS422 bus interface, and described Data Control processing module is connected to respectively GJB289A bus interface, industry ethernet interface and RS422 bus interface.
Further, described interface board is provided with AFDX bus interface, ARINC429 bus interface and RS422 interface, and described digital signal acquiring plate is connected to respectively AFDX bus interface, ARINC429 bus interface and RS422 interface.
Further, described interface board is provided with analog signal bus interface, switching signal bus interface and frequency signal bus interface; Described the first collection of simulant signal plate is connected to respectively analog signal bus interface, switching signal bus interface and frequency signal bus interface.
Further, described Data Control disposable plates includes power-on self-test module, cycle selftest module and safeguards selftest module.
Further, described Data Control disposable plates is used PowerPC processor and vxworks operating system.
the beneficial effects of the utility model are: the utility model is broken through the flight parameter acquisition system of the more limited hardware platform of existing resourceoriented, adopt the high-performance embedded hardware platform of many calculating and storage capacity, give full play to the performance of hardware, realize multiple types, the synchronous acquisition of high data volume data, receive, processing and memory function are by the combination of the harvester of use interface board and digital signal and simulating signal, make this system can gather multi-signal, comprise simulating signal, switching signal, the RS422 bus signals, the ARINC429 bus signals, the AFDX bus signals, the GJB289A bus signals, ethernet signal etc., at an equipment, realized the integrated of acquisition function, simultaneously integrated on the basis of acquisition function, increased the cache registration card that connects by bus, with this, increase quantity and the speed that data read, make real-time and the concurrent ability of system higher, simultaneously, this system has realized service data on harvester, status data and flight parameter data.
The accompanying drawing explanation
Fig. 1 is the structural drawing of a kind of aviation integrated data collection of the utility model and control system;
Fig. 2 is the structural drawing of the further specific embodiment of Fig. 1;
Fig. 3 is the embodiment of power panel in Fig. 1.
Embodiment
Below in conjunction with accompanying drawing, embodiment of the present utility model is described further:
With reference to Fig. 1, a kind of aviation integrated data gathers and control system, this system includes power panel, backboard and interface board, and described power panel is connected with respectively Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate, the second collection of simulant signal plate and indicator board; Described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to backboard by cpci bus, the output terminal of described Data Control disposable plates is connected to the input end of indicator board, and described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to interface board.
This system is unified to be connected and not only can to gather multi-signal with Data Control disposable plates and various signal acquiring board by interface board, has very strong extendability, also can simplify interface simultaneously; And the High speed rear panel bus in this system, namely cpci bus has improved data exchange capability, makes the system processing speed accelerate.
With reference to Fig. 2, be further used as preferred embodiment, described Data Control disposable plates is connected with the fast recording card that record data are provided for station earthward by the SATA bus.
This system has realized collection and writing function, an integrated fast recording card, and its capacity is not less than 64G, realizes the record of image data and reception data, and record data comprise: flight parameter data, service data, status data and voice data.The integrated reading and writing data speed of having accelerated of fast recording card in system, thus coordinate high-speed bus to improve on the whole the processing power of data.
Be further used as preferred embodiment, described fast recording card adopts reinforcement type FLASH hard disk.
The data volume of the collection of fast recording card and reception is about 1.2GB/ hour, so record the capacity that needed in 25 hours, is the 30GB left and right, therefore adopts the FLASH hard disk of 64G can meet the technical requirement of system protocol book, and reserves 46% storage space.
Because the cache registration card often need to unload record data, need frequent plug cache registration card, and common SATA connector does not possess such durability, so the SATA connector changes into other connector by card extender, select the HJ30J-18 high reliability rectangular connector of 158 factories, the HJ30J-18 transmission speed can reach 1.5Gbps, meets the SATA request signal transmission.The FLASH hard disk selects aluminium alloy to carry out the shell reinforcing, improves the reliability of product.
With reference to Fig. 3, be further used as preferred embodiment, described power panel includes normal power source input end and emergency power pack input end, and described power panel includes at least three DC voltage output ends for the internal system power supply.
With reference to Fig. 2, be further used as preferred embodiment, described interface board is provided with GJB289A bus interface, industry ethernet interface and RS422 bus interface, and described Data Control processing module is connected to respectively GJB289A bus interface, industry ethernet interface and RS422 bus interface.
Described Data Control processing module is for receiving flight parameter and the electronic device works state parameter of avionics system transmission by the GJB289A bus interface, described Data Control processing module is for receiving vibration raw data and the vibrating alert information of HUMS system by the industry ethernet interface, described Data Control processing module is for by the industry ethernet interface, the flight parameter of collection being transferred to the protection register, and described Data Control processing module is for communicating by letter with portable service equipment by the RS422 bus interface.
With reference to Fig. 2, be further used as preferred embodiment, described interface board is provided with AFDX bus interface, ARINC429 bus interface and RS422 interface, and described digital signal acquiring plate is connected to respectively AFDX bus interface, ARINC429 bus interface and RS422 interface.
Described digital signal acquiring plate is for gathering the task data of AFDX switch by the AFDX bus interface, described digital signal acquiring plate is for gathering the flight parameter of ARINC429 equipment by the ARINC429 bus interface, described digital signal acquiring plate is for gathering the flight parameter of RS422 equipment by the RS422 bus interface.
With reference to Fig. 2, be further used as preferred embodiment, described interface board is provided with analog signal bus interface, switching signal bus interface and frequency signal bus interface; Described the first collection of simulant signal plate is connected to respectively analog signal bus interface, switching signal bus interface and frequency signal bus interface.
Described the first collection of simulant signal plate is for gathering the Bus Voltage signal by the analog signal bus interface, described the first collection of simulant signal plate is for passing through the switching signal of switching signal bus interface receiving alarm control enclosure, and described the first collection of simulant signal plate is for gathering the rotor frequency signal by the frequency signal bus interface.
Described interface board is provided with the switching signal bus interface, and described the second collection of simulant signal plate is connected to the switching signal bus interface, and described the second collection of simulant signal plate is for passing through the switching signal of switching signal bus interface receiving alarm control enclosure.
With reference to Fig. 2, be further used as preferred embodiment, described Data Control disposable plates includes power-on self-test module, cycle selftest module and safeguards selftest module.
Be further used as preferred embodiment, described Data Control disposable plates is used PowerPC processor and vxworks operating system.
More than that better enforcement of the present utility model is illustrated, but the utility model is created and is not limited to described embodiment, those of ordinary skill in the art can also make all equivalents or replacement under the prerequisite without prejudice to the utility model spirit, the distortion that these are equal to or replacement all are included in the application's claim limited range.
Claims (9)
1. an aviation integrated data gathers and control system, it is characterized in that: this system includes power panel, backboard and interface board, and described power panel is connected with respectively Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate, the second collection of simulant signal plate and indicator board; Described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to backboard by cpci bus, the output terminal of described Data Control disposable plates is connected to the input end of indicator board, and described Data Control disposable plates, digital signal acquiring plate, the first collection of simulant signal plate and the second collection of simulant signal plate all are connected to interface board.
2. described a kind of aviation integrated data gathers and control system according to claim 1, and it is characterized in that: described Data Control disposable plates is connected with the fast recording card by the SATA bus.
3. described a kind of aviation integrated data gathers and control system according to claim 2, it is characterized in that: described fast recording card adopts reinforcement type FLASH hard disk.
4. described a kind of aviation integrated data gathers and control system according to claim 1, it is characterized in that: described power panel includes normal power source input end and emergency power pack input end, and described power panel includes at least three DC voltage output ends for the internal system power supply.
5. described a kind of aviation integrated data gathers and control system according to claim 1, it is characterized in that: described interface board is provided with GJB289A bus interface, industry ethernet interface and RS422 bus interface, and described Data Control disposable plates is connected to respectively GJB289A bus interface, industry ethernet interface and RS422 bus interface.
6. described a kind of aviation integrated data gathers and control system according to claim 1, it is characterized in that: described interface board is provided with AFDX bus interface, ARINC429 bus interface and RS422 interface, and described digital signal acquiring plate is connected to respectively AFDX bus interface, ARINC429 bus interface and RS422 interface.
7. described a kind of aviation integrated data gathers and control system according to claim 1, and it is characterized in that: described interface board is provided with analog signal bus interface, switching signal bus interface and frequency signal bus interface; Described the first collection of simulant signal plate is connected to respectively analog signal bus interface, switching signal bus interface and frequency signal bus interface.
8. described a kind of aviation integrated data gathers and control system according to claim 1, and it is characterized in that: described Data Control disposable plates includes power-on self-test module, cycle selftest module and safeguards selftest module.
9. described a kind of aviation integrated data gathers and control system according to claim 1, it is characterized in that: described Data Control disposable plates is used PowerPC processor and vxworks operating system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202338333U CN203299611U (en) | 2013-05-02 | 2013-05-02 | Aviation integrated-data acquisition and control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202338333U CN203299611U (en) | 2013-05-02 | 2013-05-02 | Aviation integrated-data acquisition and control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203299611U true CN203299611U (en) | 2013-11-20 |
Family
ID=49575610
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013202338333U Expired - Lifetime CN203299611U (en) | 2013-05-02 | 2013-05-02 | Aviation integrated-data acquisition and control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203299611U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103279082A (en) * | 2013-05-02 | 2013-09-04 | 广州航新航空科技股份有限公司 | Aeronautic integrated data acquisition and control system |
| CN103914044A (en) * | 2014-03-26 | 2014-07-09 | 北方信息控制集团有限公司 | Intelligent online monitoring protection device |
| CN105093146A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Low-voltage detector tester |
| WO2016184243A1 (en) * | 2015-05-15 | 2016-11-24 | 成都艾尔伯特科技有限责任公司 | Collection card for configurable io data collection system |
| CN112184950A (en) * | 2020-10-10 | 2021-01-05 | 江西洪都航空工业集团有限责任公司 | Four-card-in-one data loading recording method |
-
2013
- 2013-05-02 CN CN2013202338333U patent/CN203299611U/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103279082A (en) * | 2013-05-02 | 2013-09-04 | 广州航新航空科技股份有限公司 | Aeronautic integrated data acquisition and control system |
| CN103279082B (en) * | 2013-05-02 | 2016-02-03 | 广州航新航空科技股份有限公司 | A kind of aviation comprehensive data acquisition and control system |
| CN103914044A (en) * | 2014-03-26 | 2014-07-09 | 北方信息控制集团有限公司 | Intelligent online monitoring protection device |
| CN103914044B (en) * | 2014-03-26 | 2016-07-06 | 北方信息控制集团有限公司 | A kind of intelligent on-line monitoring protection device |
| CN105093146A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Low-voltage detector tester |
| WO2016184243A1 (en) * | 2015-05-15 | 2016-11-24 | 成都艾尔伯特科技有限责任公司 | Collection card for configurable io data collection system |
| CN112184950A (en) * | 2020-10-10 | 2021-01-05 | 江西洪都航空工业集团有限责任公司 | Four-card-in-one data loading recording method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103279082B (en) | A kind of aviation comprehensive data acquisition and control system | |
| CN203299611U (en) | Aviation integrated-data acquisition and control system | |
| CN109656473B (en) | Bridging device and method for providing proximity storage computing | |
| CN106970866A (en) | A kind of disk monitor system and method | |
| CN104239187A (en) | Hard disk state indicating device | |
| CN102508456A (en) | Backplane bus type structure of vibration monitoring and protecting device and communication control method of backplane bus type structure | |
| CN104123213A (en) | Remote SAS hard disk backboard managing system | |
| CN105095054A (en) | System and method of BMC for acquiring NVME SSD temperature information | |
| CN103107923A (en) | Fiber channel (FC) network data monitoring system and method based on system on chip (SOC) technology | |
| CN202710986U (en) | Backplane bus type structure of vibration monitoring protection device | |
| CN109032018B (en) | Unmanned aerial vehicle general signal processing device based on embedded GPU | |
| CN113885394A (en) | Airborne data comprehensive acquisition and recording system and method | |
| CN105183377B (en) | On-board data storage device | |
| CN208460081U (en) | A kind of flying quality collector | |
| CN111596599A (en) | Embedded information fusion equipment | |
| CN104361656B (en) | A kind of data logger for aviation | |
| US8874287B2 (en) | Transportable device for recording flight data | |
| Postolache et al. | IEEE 1451.4 embedded smart sensors architecture for wheelchair user monitoring | |
| CN104572515B (en) | Tracking module, method, system and on-chip system chip | |
| CN105224045A (en) | Blade server | |
| CN103391413B (en) | A kind of aerial survey image recording structure and method | |
| CN201237803Y (en) | Collection inscriber for helicopter avionics bus | |
| CN107966938A (en) | A kind of multi-medium intelligent terminal device | |
| CN210515397U (en) | Airborne quick access recorder | |
| CN210515396U (en) | Airborne protection recorder |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210121 Address after: 510700 6 / F, building 1, No.1, Guangbao Road, Guangzhou hi tech Industrial Development Zone, Guangdong Province Patentee after: Guangzhou Hangxin Aviation Technology Co.,Ltd. Address before: 510663 Guangzhou, Guangdong economic and Technological Development Zone, Science City, Cai Po Road, No. 11, C502 Patentee before: GUANGZHOU HANGXIN AVIATION TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20131120 |
|
| CX01 | Expiry of patent term |