CN208736920U - A kind of detection device of Multi Role Aircraft electric equipment - Google Patents
A kind of detection device of Multi Role Aircraft electric equipment Download PDFInfo
- Publication number
- CN208736920U CN208736920U CN201821244755.6U CN201821244755U CN208736920U CN 208736920 U CN208736920 U CN 208736920U CN 201821244755 U CN201821244755 U CN 201821244755U CN 208736920 U CN208736920 U CN 208736920U
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- detection
- cabinet
- detection device
- data
- electric equipment
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Abstract
The utility model belongs to the detection technique field of electromechanical equipment, disclose a kind of detection device of Multi Role Aircraft electric equipment, comprising: detection cabinet, instrument group, display screen, telescopic strut, solar panel, current sensor, operation button, wireless transmitter, USB interface, blower, temperature sensor, spin button.The utility model by the current sensor of setting can timely detection device current information, prevent current anomaly from causing equipment fault；By the solar energy of the available high-efficiency cleaning of the solar panel of setting, and the electric appliance by the electric energy of solar energy conversion to detection cabinet is powered, energy saving；Data can timely be will test by setting wireless transmitter and be sent to backup server, accomplish timely Backup Data, ensure data safety；It is weldingly fixed on circuit board by USB interface, the data that can be will test timely carry out backup preservation, avoid loss of data.
Description
Technical field
The utility model belongs to the detection technique field more particularly to a kind of detection of Multi Role Aircraft electric equipment of electromechanical equipment
Device.
Background technique
The development of electromechanical integration can substantially be divided into 3 stages.It is the first stage before the 1960s, this single order
Section is known as the primary stage.In this period, people consciously unconsciously improve mechanical produce using the initial achievements of electronic technology
The performance of product.Especially during World War II, war have stimulated the combination of engineering goods and electronic technology, these machines
The military technology being electrically coupled, switchs to civilian after the war, has served to the recovery of post-war economic positive.At that time develop and develop from
On the whole also in autonomous state.Since certain level, mechanical technique and electronics has not yet been reached in the development of electronic technology at that time
The combination of technology can not also extensively develop, and the product developed also can not large-scale popularization.However, existing electromechanics is set
Standby detection device is powered by traditional approach expends electric energy；Alarm cannot be detected in time to electromechanical equipment electric current, be easy to cause
Safety accident；The data of detection cannot be backed up timely simultaneously, be easy to cause loss of data.
In conclusion problem of the existing technology is:
(1) detection device of existing electromechanical equipment is powered by traditional approach expends electric energy；It cannot be to electromechanical equipment electric current
Detection alarm in time, be easy to cause safety accident.
(2) data detected cannot be backed up timely, be easy to cause loss of data.
Utility model content
In view of the problems of the existing technology, the utility model provides a kind of detection device of Multi Role Aircraft electric equipment.
The utility model is realized in this way a kind of detection device of Multi Role Aircraft electric equipment is provided with detection cabinet, inspection
Cabinet is surveyed by being embedded with current sensor, wireless transmitter has been screwed above detection machine right end, detection cabinet is logical
It crosses telescopic rod and is fixed with solar panel；
By the current sensor of setting can timely detection device current information, prevent current anomaly from causing equipment
Failure；By the solar energy of the available high-efficiency cleaning of the solar panel of setting, and by the electric energy of solar energy conversion to inspection
The electric appliance for surveying cabinet is powered, energy saving；By be arranged wireless transmitter can timely will test data be sent to it is standby
Part server, accomplishes timely Backup Data, ensures data safety.
Further, USB interface is fixed on detection cabinet by inserting, and USB interface is connect by data line with single-chip microcontroller；
It is weldingly fixed on circuit board by USB interface, the data that can be will test timely carry out backup preservation, avoid making
At loss of data.
Further, blower is bolted on the outside of detection cabinet, and temperature sensor is fixed by screws in detection machine
Case upper right side, fan switch and temperature sensor are connect by data line with single-chip microcontroller；
Single-chip microcontroller is connected with temperature sensor by setting blower, can cool down automatically to detection device, keep detection dress
Set the constant of internal temperature.
Further, detection cabinet upper end has been bolted telescopic strut；
By the way that telescopic rod is arranged, the height of adjustable solar panel receives solar panel preferably too
Sunlight.
Detailed description of the invention
Fig. 1 is the structure of the detecting device schematic diagram of Multi Role Aircraft electric equipment provided by the embodiment of the utility model.
Fig. 2 is detection cabinet schematic diagram of internal structure provided by the embodiment of the utility model.
Fig. 3 is Telescopic rod structure schematic diagram provided by the embodiment of the utility model.
Fig. 4 is wireless transmitter, current sensor and temperature sensor and single-chip microcontroller provided by the embodiment of the utility model
Connection circuit diagram.
Fig. 5 is fan circuit figure provided by the embodiment of the utility model.
Fig. 6 is electromagnetic valve circuit figure provided by the embodiment of the utility model.
In figure: 1, detecting cabinet；2, instrument group；3, display screen；4, telescopic strut；5, solar panel 6, current sense
Device；7, operation button；8, wireless transmitter；9, USB interface；10, blower；11, temperature sensor；12, spin button.
Specific embodiment
For the invention, features and effects that can further appreciate that the utility model, the following examples are hereby given, and cooperates
Detailed description are as follows for attached drawing.
The structure of the utility model is explained in detail with reference to the accompanying drawing.
As shown in figs 1 to 6, the detection device of Multi Role Aircraft electric equipment provided by the utility model include: detection cabinet 1,
Instrument group 2, display screen 3, telescopic strut 4, solar panel 5, current sensor 6, operation button 7, wireless transmitter 8, USB
Interface 9, blower 10, temperature sensor 11, spin button 12.
It detects cabinet 1 and is passed through by being embedded with current sensor 6, instrument group 2, display screen 3, operation button 7, instrument group 2
Data line is connect with display screen 3, and wireless transmitter 8 has been screwed above detection 1 right end of cabinet, and detection cabinet 1 passes through
Telescopic strut 4 is fixed with solar panel 5, and detection 1 upper end of cabinet has been bolted telescopic strut 4, and telescopic strut 4 is logical
Bolt and solar panel 5 are crossed, spin button 12 is fixed on telescopic strut 4 by thread helix, and USB interface 9 passes through inserting
It is fixed on detection cabinet 1, blower 10 is bolted on 1 outside of detection cabinet, and temperature sensor 11 is screwed
In detection 1 upper right side of cabinet, the switch of blower 10 and temperature sensor 11 are connect by data line with single-chip microcontroller, wireless transmitter 8,
USB interface 9 and current sensor 6 are connect by data line with single-chip microcontroller, and single-chip microcontroller passes through data line and Multi Role Aircraft electric equipment
Detection device general supply electromagnetic valve switch connection, blower 10 connected to power supply by conducting wire.
Single chip computer AT DA pin in wireless transmitter 8 is connect with (AD0) P0.0 pin in 80C320 single-chip microcontroller, wirelessly
Single-chip microcontroller VCC pin in transmitter 8 is connect with the VCC in 80C320 single-chip microcontroller.- HT pin in current sensor circuit with
P1.2/RXD1 pin connection in 80C320 single-chip microcontroller ,+HT pin are connect with the P1.3TXD1 pin in 80C320 single-chip microcontroller.
The SERVO pin of J300 single-chip microcontroller is connect with (A8) P2.0 pin in 80C320 single-chip microcontroller in blower 7.I/O in solenoid valve
Line is connect with P1.0 (I/O) pin in single-chip microcontroller.
When the utility model is used, change the height of solar panel 5 by telescopic strut 4, solar panel 5 will
The electric energy of solar energy conversion is powered to the electric appliance of detection cabinet 1；Staff can be operated by operation button 7；
Instrument group 2 shows the Measurement And Control of The Jet Flotation Column of inspection by display screen 3, by USB interface 9, to the data of detection timely into
Row backup.If checking 1 current anomaly of cabinet, current sensor 6 detects current anomaly, signal is transmitted to single-chip microcontroller, monolithic
Machine issues instruction.The electromagnetic valve switch for controlling the detection device general supply of Multi Role Aircraft electric equipment is powered off, temperature sensor
Temperature inside the detection device of 11 detection electromechanical equipments, if temperature is excessively high, data are transmitted to single-chip microcontroller by temperature sensor 11, single
Piece machine issues instruction, and starting blower 10 is switched, radiated to detection device inside.
The above is only the preferred embodiment to the utility model, is not made in any form to the utility model
Limitation, it is all according to the technical essence of the utility model any simple modification made to the above embodiment, equivalent variations with
Modification, is all within the scope of the technical scheme of the utility model.
Claims (4)
1. a kind of detection device of Multi Role Aircraft electric equipment, which is characterized in that the detection device of the Multi Role Aircraft electric equipment
It is provided with
Detect cabinet；
Cabinet is detected by being embedded with current sensor, wireless transmitter has been screwed above detection machine right end, has detected
Cabinet is fixed with solar panel by telescopic rod.
2. the detection device of Multi Role Aircraft electric equipment as described in claim 1, which is characterized in that USB interface is solid by inserting
It is scheduled on detection cabinet, USB interface is connect by data line with single-chip microcontroller.
3. the detection device of Multi Role Aircraft electric equipment as described in claim 1, which is characterized in that blower is bolted on
It detects on the outside of cabinet, temperature sensor is fixed by screws in detection cabinet upper right side, and fan switch and temperature sensor pass through
Data line is connect with single-chip microcontroller.
4. the detection device of Multi Role Aircraft electric equipment as described in claim 1, which is characterized in that detection cabinet upper end passes through spiral shell
Bolt is fixed with telescopic rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821244755.6U CN208736920U (en) | 2018-08-02 | 2018-08-02 | A kind of detection device of Multi Role Aircraft electric equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821244755.6U CN208736920U (en) | 2018-08-02 | 2018-08-02 | A kind of detection device of Multi Role Aircraft electric equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208736920U true CN208736920U (en) | 2019-04-12 |
Family
ID=66029466
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821244755.6U Expired - Fee Related CN208736920U (en) | 2018-08-02 | 2018-08-02 | A kind of detection device of Multi Role Aircraft electric equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208736920U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111082390A (en) * | 2020-01-09 | 2020-04-28 | 南京亚派软件技术有限公司 | Electromechanical device fault positioning alarm device |
| WO2022077667A1 (en) * | 2020-10-15 | 2022-04-21 | 苏州莱锦机电自动化有限公司 | Electromechanical monitoring device |
-
2018
- 2018-08-02 CN CN201821244755.6U patent/CN208736920U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111082390A (en) * | 2020-01-09 | 2020-04-28 | 南京亚派软件技术有限公司 | Electromechanical device fault positioning alarm device |
| WO2022077667A1 (en) * | 2020-10-15 | 2022-04-21 | 苏州莱锦机电自动化有限公司 | Electromechanical monitoring device |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190412 Termination date: 20200802 |