CN207182084U - A kind of device for being used to test flight control computer - Google Patents
A kind of device for being used to test flight control computer Download PDFInfo
- Publication number
- CN207182084U CN207182084U CN201720988173.8U CN201720988173U CN207182084U CN 207182084 U CN207182084 U CN 207182084U CN 201720988173 U CN201720988173 U CN 201720988173U CN 207182084 U CN207182084 U CN 207182084U
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- China
- Prior art keywords
- rack
- front panel
- test
- greeve controller
- zero
- 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 - Fee Related
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- Testing Electric Properties And Detecting Electric Faults (AREA)
Abstract
The utility model discloses a kind of device for being used to test flight control computer, mainly solves the problems such as testing process existing for prior art is complicated and the huge clumsiness of equipment is not easily shifted.The device includes rack, product bracket in rack, Zero greeve controller on product bracket, Signal-regulated kinase, aircraft sensors module, the power supply module being connected on product bracket and with Zero greeve controller, it is arranged on the radiator fan of enclosure top, the roller of rack bottom is arranged on, is arranged on power switch, the test interface for being used for power supply module on rack front panel, is arranged on the ammeter for being used for display test equipment supply current on rack front panel.By such scheme, purpose that the utility model has reached convenient test and has been be easily moved has very high practical value and promotional value.
Description
Technical field
It the utility model is related to aircraft control system testing field, and in particular to a kind of dress for being used to test flight control computer
Put.
Background technology
With the rapid development of aeronautical technology, control theory, fault-toleranr technique and emulation technology, flight control technology has
Very big raising, and penetrated into industrial production and the various aspects of military field engineering.Flight control computer is whole flight control
The core of system, it is main to complete control rate calculating, redundancy management, BIT (built in test survey), system call, fault detect, vacant
The crucial special task such as rate reconstruct, therefore have extremely important meaning to the test of its various functions.Test equipment can be to flying
Real-time, availability, stability and the reliability of control system carry out complete test.
Flight control computer has the characteristics that high to software and hardware reliability requirement, signal kinds are various, and will to real-time
Ask high, cause its testing process extremely complex.Most bulky not easily shifted, the cost of implementation of traditional winged control test equipment
Height, software portability are low.Meanwhile in order to carry out data path test to tested flight control computer, very high is required to board, is needed
The interface division equipment resource of test product can be simulated.
Utility model content
The purpose of this utility model is to provide a kind of equipment for testing flight control computer mainly solve prior art
Present in testing process is complicated, requires high to test component and the problems such as the huge clumsiness of equipment is not easily shifted.
To achieve these goals, the technical solution adopted in the utility model is as follows：
A kind of device for being used to test flight control computer, including rack, the product bracket in rack, installed in production
Zero greeve controller on product carrier, the Signal-regulated kinase being connected on product bracket and with Zero greeve controller, is arranged on
The aircraft sensors module being connected on product bracket and with Zero greeve controller, connect on product bracket and with Zero greeve controller
The power supply module connect, four be arranged on enclosure top be used for radiate and the radiator fan that is connected with power supply module, be arranged on rack
On the angle of bottom four and for mobile roller, it is arranged on rack front panel and is used for power supply module and connects with Zero greeve controller
The power switch connect, the test interface for being arranged on rack front panel and being connected with Zero greeve controller, is arranged on side of cabinet plate
Serial ports that is upper and being connected with Zero greeve controller, the computer being connected with serial ports, the mouse being connected with serial ports；The aircraft sensors mould
Block includes the discrete magnitude input module being connected with test interface, the Analog input mModule being connected with test interface, connects with serial ports
The discrete magnitude output module connect, the analog output module being connected with serial ports；The power supply module includes being arranged on before rack
The voltmeter being connected on plate with Zero greeve controller, and be arranged on rack front panel and be connected ammeter with Zero greeve controller.
Further, the rack front panel is provided with the printer being connected with computer.
Specifically, the rack front panel is provided with the handle for being used for opening front panel.
Compared with prior art, the utility model has the advantages that：
(1) test equipment of the utility model design, by serial ports connecting test equipment, Zero greeve controller is surveyed with outside
Examination equipment is tested, and the voltmeter and ammeter set on rack front panel in time, accurately can show that test is set
Standby magnitude of voltage and current value, it can intuitively check whether to go wrong.
(2) bracket set in the utility model rack facilitates putting for internal components, while set on rack top plate
Four radiator fans can shed heat caused by device work in rack so that device will not burn because of overheating itself
Bad component and influence to use.
(3) four rolling that the utility model is arranged in bottom four corners can facilitate the movement of test equipment, set simultaneously
Printer on front panel can out achieve important data-printing, be consulted after convenient.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the utility model interior of equipment cabinet structural representation.
Fig. 3 is work block diagram of the present utility model.
In above-mentioned accompanying drawing, component names are as follows corresponding to reference：
1- racks, 2- brackets, 3- Zero greeve controllers, 4- Signal-regulated kinases, 5- aircraft sensors modules, 6- power supply moulds
Block, 7- radiator fans, 8- rollers, 9- power switches, 10- test interfaces, 11- serial ports, 12- computers, 13- mouses, 14- discrete magnitudes
Input module, 15- Analog input mModules, 16- discrete magnitude output modules, 17- analog output modules, 18- voltmeters, 19-
Ammeter, 20- printers, 21- handles.
Embodiment
The utility model is described in further detail with reference to the accompanying drawings and examples, and embodiment of the present utility model includes
But it is not limited to the following example.
Embodiment
A kind of device for being used to test flight control computer, including rack 1, the product bracket 2 in rack 1, installation
Zero greeve controller 3 on product bracket 2, the Signal-regulated kinase being connected on product bracket 2 and with Zero greeve controller 3
4, the aircraft sensors module 5 being connected on product bracket 2 and with Zero greeve controller 3, on product bracket 2 and with
The power supply module 6 that Zero greeve controller 3 connects, four are arranged on the radiator fan 7 that the top of rack 1 is used to radiate, and are arranged on rack 1
On the angle of bottom four and it is used for mobile roller 8, is arranged on the power switch 9 for being used for power supply module 6 on the front panel of rack 1, if
The test interface 10 put on the front panel of rack 1 and be connected with Zero greeve controller 3, be arranged on the side panel of rack 1 and with zero groove
The serial ports 11 that controller 3 connects, the computer 12 being connected with serial ports 11, the mouse 13 being connected with serial ports；The aircraft sensors mould
Block 5 is including the discrete magnitude input module 14 being connected with test interface 10, the Analog input mModule 15 being connected with test interface 10,
The discrete magnitude output module 16 being connected with serial ports 11, the analog output module 17 being connected with serial ports 11；The power supply module 6 wraps
The voltmeter 18 for being arranged on and being connected on the front panel of rack 1 with Zero greeve controller 3 is included, and is arranged on the front panel of rack 1 and zero
Greeve controller 3 connects ammeter 19.
Also, the front panel of rack 1 is provided with the printer 20 being connected with computer 12, is set on the front panel of rack 1
There is the handle 21 for opening front panel.
Before test, mouse 13 and computer 12 are accessed into serial ports 11, test lead access test interface 10, are then turned on power supply
Switch 9, now Zero greeve controller 3, Signal-regulated kinase 4, aircraft sensors module 5, power supply module 6 fully enter Working mould
Formula, Signal-regulated kinase 4 are transferred to signal, and test end signal is through the discrete magnitude input module in aircraft sensors module 5
14th, signal is transferred in Zero greeve controller 3 by Analog input mModule 15 by signal wire, then the feedback letter of Zero greeve controller 3
Breath is transmitted signal by serial ports 11 through the discrete magnitude output module 16 in aircraft sensors module 5, analog output module 17
Onto computer 12, while magnitude of voltage and electricity when the voltmeter 18 on the front panel of rack 1 and ammeter 19 will show current test
Flow valuve, and can intuitively know whether voltage is normal with electric current, and mouse can be passed through to the information being shown on computer 12
13 choose, and are then printed and achieved by the printer 20 being connected with computer 12, convenient to consult.
Also, 4 radiator fans 7 that the top of rack 1 is set are to the Zero greeve controller 3 on the bracket 2 of rack 1, letter
Number conditioning module 4, aircraft sensors module 5, power supply module 6 are radiated, ensure device will not because operating temperature is too high and
Influence normal work is burnt, while the roller 8 being arranged on the angle of rack 1 bottom four, it can facilitate the movement of test device,
And the handle 21 on the front panel of rack 1 can open front panel, the device in rack 1 can be changed..
Above-described embodiment is only preferred embodiment of the present utility model, not to the limitation of scope of protection of the utility model,
In every case design principle of the present utility model, and the change for carrying out non-creativeness work on this basis and making are used, all should
Belong within the scope of protection of the utility model.
Claims (3)
- A kind of 1. device for being used to test flight control computer, it is characterised in that including rack (1), the production in rack (1) Product carrier (2), the Zero greeve controller (3) on product bracket (2), controlled on product bracket (2) and with zero groove The Signal-regulated kinase (4) of device (3) connection, the aircraft sensing being connected on product bracket (2) and with Zero greeve controller (3) Device module (5), the power supply module (6) being connected on product bracket (2) and with Zero greeve controller (3), is arranged on rack (1) Top and the radiator fan (7) being connected with power supply module (6), it is arranged on rack (1) bottom and is used for mobile roller (8), setting It is used for power supply module (6) and the power switch (9) being connected with Zero greeve controller (3) on rack (1) front panel, is arranged on machine The test interface (10) being connected on cabinet (1) front panel and with Zero greeve controller (3), it is arranged on rack (1) side panel and with zero The serial ports (11) of greeve controller (3) connection, the computer (12) being connected with serial ports (11), the mouse being connected with serial ports (13)；It is described Aircraft sensors module (5) includes the discrete magnitude input module (14) being connected with test interface (10), with test interface (10) even The Analog input mModule (15) connect, the discrete magnitude output module (16) being connected with serial ports (11), the mould being connected with serial ports (11) Analog quantity output module (17)；The power supply module (6) includes being arranged on rack (1) front panel being connected with Zero greeve controller (3) Voltmeter (18), and be arranged on rack (1) front panel and be connected ammeter (19) with Zero greeve controller (3).
- A kind of 2. device for being used to test flight control computer according to claim 1, it is characterised in that the rack (1) Front panel is provided with the printer (20) being connected with computer (12).
- A kind of 3. device for being used to test flight control computer according to claim 1, it is characterised in that the rack (1) Front panel is provided with the handle (21) for being used for opening front panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720988173.8U CN207182084U (en) | 2017-08-09 | 2017-08-09 | A kind of device for being used to test flight control computer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720988173.8U CN207182084U (en) | 2017-08-09 | 2017-08-09 | A kind of device for being used to test flight control computer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207182084U true CN207182084U (en) | 2018-04-03 |
Family
ID=61745629
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720988173.8U Expired - Fee Related CN207182084U (en) | 2017-08-09 | 2017-08-09 | A kind of device for being used to test flight control computer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207182084U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108825530A (en) * | 2018-06-21 | 2018-11-16 | 郑州云海信息技术有限公司 | A kind of fan board |
| CN110362067A (en) * | 2019-07-20 | 2019-10-22 | 成都飞机工业（集团）有限责任公司 | Actuator performance tester and test method on a kind of machine |
-
2017
- 2017-08-09 CN CN201720988173.8U patent/CN207182084U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108825530A (en) * | 2018-06-21 | 2018-11-16 | 郑州云海信息技术有限公司 | A kind of fan board |
| CN110362067A (en) * | 2019-07-20 | 2019-10-22 | 成都飞机工业（集团）有限责任公司 | Actuator performance tester and test method on a kind of machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180403 Termination date: 20190809 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |