CN207946502U - A kind of aviation contactor test device - Google Patents
A kind of aviation contactor test device Download PDFInfo
- Publication number
- CN207946502U CN207946502U CN201820413954.9U CN201820413954U CN207946502U CN 207946502 U CN207946502 U CN 207946502U CN 201820413954 U CN201820413954 U CN 201820413954U CN 207946502 U CN207946502 U CN 207946502U
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- China
- Prior art keywords
- communicator
- contactor
- test device
- controller
- display
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- 238000012360 testing method Methods 0.000 title claims abstract description 50
- 238000005259 measurement Methods 0.000 claims abstract description 29
- 238000004891 communication Methods 0.000 claims description 17
- 238000009413 insulation Methods 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
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- Testing Electric Properties And Detecting Electric Faults (AREA)
Abstract
The utility model provides a kind of aviation contactor test device, including test main frame and tester, the test main frame includes cabinet, controller, display, first communicator, data collector, and first power supply, the tester includes engine base, second communicator, second source, data pre-processor, measurement assembly, and measure contact folder, when being measured to contactor, folder is contacted by the measurement being arranged on the contactor, directly device can be clamped on contactor and be measured, it need to will only be measured after clamping finishes and contact folder release, avoiding phase before testing carries out cumbersome wiring to contactor and prepares and avoid after a test to take out stitches to equipment, greatly reduce test preparatory process, testing efficiency is greatly speeded up.
Description
Technical field
The utility model is related to test device fields, more particularly to a kind of aviation contactor test device.
Background technology
In aviation field, in order to ensure the safety of aircraft in the sky, it is provided with numerous electrical equipments, wherein including just
Contactor.Contactor is for frequently switching on or off operating current and for switching on or off current flow at a distance
The power supply of machine.Since the quality of AC vacuum contactor determines the reliability electrically bribed, it is therefore desirable to be connect to AC vacuum
The performance of tentaculum is tested.But multimeter is mostly used greatly for the test of the performance of contactor at present and is waited for detect
Device is surveyed, directly detection measures the parameters such as the current resistor of contactor.But contactor is connected manually using multimeter
Performance test, single test need to carry out wiring to contact, also need to take out stitches after being completed, connecing repeatedly is torn open
Tedious process, and inefficiency interfere the quick progress of test.
Utility model content
In order to overcome defect in the prior art, the technical problem to be solved by the utility model is to propose that a kind of aviation connects
Tentaculum test device tears test line procedures open without carrying out cumbersome connecing, you can rapidly to carry out clamping test to tester,
The front and back activity time of test is reduced, testing efficiency is accelerated.
For this purpose, the utility model uses following technical scheme：
The utility model provides a kind of aviation contactor test device, including test main frame and tester, the survey
Examination host includes cabinet, controller, display, the first communicator, data collector and the first power supply, the display edge
Embedded in the front end face of the cabinet, the controller, the data collector and first power supply may be contained within the machine
The inside of case, first communicator are fixed on the top of the cabinet, the controller respectively with the display, the number
It is electrically connected according to collector and first power supply, the data collector is also electrically connected with first communicator, institute
Tester is stated to include engine base, the second communicator, second source, data pre-processor, measurement assembly and measure contact folder, institute
State measurement contact it is clamping due to the top of the engine base, second communicator is fixed on the bottom of the engine base, the data
Preprocessor, the second source, the measurement assembly may be contained within the inside of the engine base, the data pre-processor difference
It is electrically connected with the measurement assembly, second communicator, the second source, the measurement assembly is contacted with the measurement
Folder is electrically connected, and first communicator is electrically connected with second communicator by communication cable.
In the utility model preferably technical solution, the measurement assembly includes voltage sensor and current sense
Device.
In the utility model preferably technical solution, the display is configured to show with the touch of touch input
Screen.
In the utility model preferably technical solution, it is all provided with inside first communicator and second communicator
There are wifi communication modules, the GSM communication modules of interconnection, is respectively provided on first communicator and second communicator
There is communication antenna.
In the utility model preferably technical solution, the controller is configured to programmable logic controller (PLC).
In the utility model preferably technical solution, it is provided with metal contact block on the collet for measuring contact folder,
It is provided with insulation rubber sleeve on the measurement contact folder.
In the utility model preferably technical solution, first power supply and the second source are each configured to lithium electricity
Pond.
The beneficial effects of the utility model are：
A kind of aviation contactor test device provided by the utility model, when being measured to contactor, by connecing
Device, can directly be clamped on contactor and measure, after clamping finishes only by the measurement contact folder being arranged on tentaculum
It need to will measure and contact folder release, the phase before testing that avoids carries out cumbersome wiring preparation to contactor and avoids
It takes out stitches to equipment after test, greatly reduces test preparatory process, greatly speeded up testing efficiency.
Description of the drawings
Fig. 1 is the structural schematic diagram for the aviation contactor test device that specific embodiment of the present invention provides.
In figure：
1, test main frame, 2, tester, 11, cabinet, 12, controller, 13, display, the 14, first communicator, 15, data
Collector, the 16, first power supply, 17, communication antenna, 21, engine base, the 22, second communicator, 23, second source, 24, measurement assembly,
25, data pre-processor, 26, measure contact folder, 27, insulation rubber sleeve, 28, metal contact block, 241, voltage sensor, 242,
Current sensor, 3, communication cable.
Specific implementation mode
Further illustrate the technical solution of the utility model below with reference to the accompanying drawings and specific embodiments.
As shown in Figure 1, a kind of aviation contactor test device is provided in embodiment, including test main frame 1 and test
Device 2, test main frame 1 include cabinet 11, controller 12, display 13, the first communicator 14, data collector 15 and first
Power supply 16, display 13 are embedded in the front end face of cabinet 11, and controller 12, data collector 15 and the first power supply 16 are all provided with
It is placed in the inside of cabinet 11, the first communicator 14 is fixed on the top of cabinet 11, and controller 12 is adopted with display 13, data respectively
Storage 15 and the first power supply 16 are electrically connected, and data collector 15 is also electrically connected with the first communicator 14, and tester 2 includes
Engine base 21, the second communicator 22, second source 23, data pre-processor 25, measurement assembly 24 and measurement contact folder 26, are surveyed
The tops that amount contact folder 26 is fixed on engine base 21, the second communicator 22 are fixed on the bottom of engine base 21, data pre-processor 25, the
Two power supplys 23, measurement assembly 24 may be contained within the inside of engine base 21, and data pre-processor 25 is logical with measurement assembly 24, second respectively
Device 22, the electric connection of second source 23 are interrogated, measurement assembly 24 contacts folder 26 with measurement and is electrically connected, the first communicator 14 and second
Communicator 22 is electrically connected by communication cable 3.Tester 2 is responsible for connection aviation contactor, and test main frame 1 is then responsible for reception
Carry out the data that tester 2 is transmitted, carries out processing and show.When starting test, by 26 dozens, measurement contact folder in tester 2
It opens, is clamped to the contactor to be measured and contacts on contact accordingly, so that it may to detect the performance of contactor, such as electricity
Stream, voltage and resistance etc..It measures contact folder 26 with measurement assembly 24 to be connected, measurement assembly 24 is detected by from measurement contact folder
26 electric currents transmitted, and then by the data transmission detected to data pre-processor 25, data pre-processor 25 will monitor number
According to being handled.Then data are transmitted to by the second communicator 22 in the first communicator 14 in test main frame 1, first is logical
News device 14, which is received from tester 2, is transmitted through the data come, and is then delivered in data collector 15, data collector 15 is by data
It is handled, will be in treated data transmission to controller 12, then display 13 is presented in data processing by controller 12
In, tester can easily read the parameters of contactor by observing display 13, whether learn contactor
It is intact.First power supply 16 is respectively that test main frame 1 and tester 2 provide power supply with second source 23.
In order to easily measure the parameters of contactor, further, measurement assembly 24 include voltage sensor 241 with
And current sensor 242, it can be tested out through contactor respectively by voltage sensor 241 and current sensor 242
Voltage, electric current, to learn whether it is normal, while controller 12 is according to pre-set calculation formula, using measuring
Voltage value and current value can obtain the resistance value of contactor.
In order to send control instruction to contactor test device, further, display 13 is configured to can be with touch input
Touch display screen.Every data parameters of contactor can be clearly observed by 13 one side of display, on the other hand
Touch input can be carried out, control shows different parameters.
In order to facilitate the contactor of test different location, further, in the first communicator 14 and the second communicator 22
Portion is equipped with the wifi communication modules of interconnection, GSM communication modules, is all provided on the first communicator 14 and the second communicator 22
It is equipped with communication antenna 17.In addition to conventional communication cable 3 connects between first communicator 14 and the second communicator 22, can pass through
Wifi and GSM communicates wirelessly connection, when communication cable 3 falls short of, can remove communication cable 3, allow tester 2 with
The scope of application of test device is widened in wireless telecommunications between test main frame 1.
Multi-functional control is carried out to test device in order to realize, further, controller 12 is configured to programmable logic control
Device processed.
In order to accurately detect contactor arrangement, further, measures and be provided with metal contact on the collet of contact folder 26
Block 28 measures and is provided with insulation rubber sleeve 27 on contact folder 26.Metal contact block 28 is connected with the contact of contactor, receives to come from
Electric signal on contactor.Simultaneously measure contact folder 26 on be arranged insulation rubber sleeve 27, avoid manually connect pull out when, by
In the parameter that the Resistance Influence of human hand measures.
In order to enable the continuation of the journey of detection device is lasting, further, the first power supply 16 and second source 23 are each configured to
Lithium battery, lithium battery has high storage energy density, while service life is very long, is suitble to be used in and is powered herein.
The utility model is described with reference to the preferred embodiments, and those skilled in the art know, is not departing from this reality
In the case of with novel spirit and scope, various changes or equivalence replacement can be carried out to these features and embodiment.This reality
It is not limited to the particular embodiment disclosed with novel, other embodiments fallen into claims hereof all belong to
In the range of the utility model protection.
Claims (7)
1. a kind of aviation contactor test device, it is characterised in that：Including test main frame (1) and tester (2), the test
Host (1) include cabinet (11), controller (12), display (13), the first communicator (14), data collector (15) and
First power supply (16)；
The display (13) is embedded in the front end face of the cabinet (11), the controller (12), the data collector
(15) and first power supply (16) may be contained within the inside of the cabinet (11), and first communicator (14) is fixed on
The top of the cabinet (11)；
The controller (12) respectively with the display (13), the data collector (15) and first power supply (16)
It is electrically connected；
The data collector (15) is also electrically connected with first communicator (14)；
The tester (2) includes engine base (21), the second communicator (22), second source (23), data pre-processor (25), surveys
It measures component (24) and measures contact folder (26)；
The top for measuring contact folder (26) and being fixed on the engine base (21), second communicator (22) are fixed on the machine
The bottom of seat (21), the data pre-processor (25), the second source (23), the measurement assembly (24) may be contained within institute
State the inside of engine base (21)；
The data pre-processor (25) respectively with the measurement assembly (24), second communicator (22), it is described second electricity
Source (23) is electrically connected；
The measurement assembly (24) contacts folder (26) with the measurement and is electrically connected；
First communicator (14) is electrically connected with second communicator (22) by communication cable (3).
2. a kind of aviation contactor test device according to claim 1, it is characterised in that：
The measurement assembly (24) includes voltage sensor (241) and current sensor (242).
3. a kind of aviation contactor test device according to claim 1, it is characterised in that：
The display (13) is configured to can be with the touch display screen of touch input.
4. a kind of aviation contactor test device according to claim 1, it is characterised in that：
Be equipped with inside first communicator (14) and second communicator (22) interconnection wifi communication modules,
GSM communication modules；
It is both provided with communication antenna (17) on first communicator (14) and second communicator (22).
5. a kind of aviation contactor test device according to claim 1, it is characterised in that：
The controller (12) is configured to programmable logic controller (PLC).
6. a kind of aviation contactor test device according to claim 1, it is characterised in that：
It is provided with metal contact block (28) on the collet for measuring contact folder (26)；
It is provided with insulation rubber sleeve (27) on the measurement contact folder (26).
7. a kind of aviation contactor test device according to claim 1, it is characterised in that：
First power supply (16) and the second source (23) are each configured to lithium battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820413954.9U CN207946502U (en) | 2018-03-26 | 2018-03-26 | A kind of aviation contactor test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820413954.9U CN207946502U (en) | 2018-03-26 | 2018-03-26 | A kind of aviation contactor test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207946502U true CN207946502U (en) | 2018-10-09 |
Family
ID=63698340
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820413954.9U Active CN207946502U (en) | 2018-03-26 | 2018-03-26 | A kind of aviation contactor test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207946502U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112904194A (en) * | 2021-02-24 | 2021-06-04 | 江西昌柘伟业航空装备技术有限公司 | Aircraft relay ground test method |
-
2018
- 2018-03-26 CN CN201820413954.9U patent/CN207946502U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112904194A (en) * | 2021-02-24 | 2021-06-04 | 江西昌柘伟业航空装备技术有限公司 | Aircraft relay ground test method |
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