CN208705701U - A kind of aircraft air source truck electrical control gear - Google Patents
A kind of aircraft air source truck electrical control gear Download PDFInfo
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- CN208705701U CN208705701U CN201821443418.XU CN201821443418U CN208705701U CN 208705701 U CN208705701 U CN 208705701U CN 201821443418 U CN201821443418 U CN 201821443418U CN 208705701 U CN208705701 U CN 208705701U
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- 238000004891 communication Methods 0.000 claims description 18
- 238000012544 monitoring process Methods 0.000 claims description 18
- 230000005611 electricity Effects 0.000 claims description 10
- 230000007257 malfunction Effects 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 8
- 238000009434 installation Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 3
- 230000010354 integration Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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- 101100449818 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) ECM4 gene Proteins 0.000 description 1
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Abstract
The utility model discloses a kind of aircraft air source truck electrical control gears, the power distribution module for including: carrier body and being arranged on carrier body, man-machine interface, master controller, main interface, input module and output module, main interface with external main power source for connecting, power distribution module for giving man-machine interface respectively, master controller, input module and output module power supply, man-machine interface is connect by CAN bus with master controller, master controller by main interface with outside signal transducer connect master controller also respectively with input module, output module connection, input module is connect with output module, output module is connect with main interface.The integrated level of device is improved on carrier body by the way that corresponding electrical component to be integrally disposed in, all maintenance and operation parts are wherein preferably arranged in the one side of carrier body, be conducive to operation and in time discovery failure and maintenance failure, it is connect additionally by a main interface with complete machine, so that installation and replacement are simple and convenient.
Description
Technical field
The utility model relates to aircraft air source truck technical field, in particular to a kind of aircraft air source truck electrical control gear.
Background technique
Aircraft air source truck is to provide the ground of compressed air by Diesel Driven for aircraft engine starting or air-conditioning system
Equipment.
The electrical system of aircraft air source truck mainly by starting control, operating parameter monitoring, compressor mode selection with control,
The compositions such as controlling alarm, shutdown control and man-machine interface.
With the continuous intensification of the electrical integration degree of aircraft air source truck, the normal use of air source truck is depended entirely on electrically
How the normal use of system is quickly found out fault point, checks failure problems in time once electrical system breaks down, or
Quick-replaceable failure part becomes aircraft air source truck problem most important at present.
Utility model content
In view of this, can be improved electricity the purpose of the utility model is to provide a kind of aircraft air source truck electrical control gear
The convenience of gas control device maintenance.
To achieve the above object, the utility model provides the following technical solutions:
A kind of aircraft air source truck electrical control gear, comprising: carrier body and the power supply being arranged on the carrier body
Distribution module, man-machine interface, master controller, main interface, input module and output module, the main interface are used for and external main electricity
Source connection, the main interface are also connect with the power distribution module, and the power distribution module is for respectively to described man-machine
Interface, the master controller, the input module and output module power supply, the man-machine interface pass through CAN bus and the master
Controller connection, the master controller are connect by the main interface with external signal transducer, and the master controller also divides
It is not connect with the input module, the output module, the input module is connect with the output module, the output module
It is connect with the main interface.
Preferably, be additionally provided with communication interface on the carrier body, the communication interface respectively with the power distribution mould
Block is connected with the CAN bus.
Preferably, the power distribution module, the man-machine interface, the master controller, the input module and output
Module is arranged on the same face of the carrier body.
Preferably, the main interface is connect with the CAN bus.
Preferably, the power distribution module include power supply main road and it is multiple with the man-machine interface, the master controller,
The input module, output module power supply and the main interface and the communication interface are powered branch correspondingly.
It preferably, further include monitoring module, the monitoring module is for monitoring the power supply main road and each confession in real time
Electric branch uses electricity condition and malfunction.
Preferably, the monitoring module includes alarm module, and the alarm module is used to work as the power supply main road or described
It is issued warning signal when the not enough power supply for branch of powering, fault-signal is issued when breaking down.
Preferably, the monitoring module is connect with the CAN bus.
Compared with prior art, above-mentioned technical proposal has the advantage that
A kind of aircraft air source truck electrical control gear provided by the utility model, comprising: carrier body and setting are carrying
Power distribution module, man-machine interface, master controller, main interface, input module and output module on body component, main interface are used for
It is connect with external main power source, power distribution module to man-machine interface, master controller, input module and output module for supplying respectively
Electricity, man-machine interface are connect by CAN bus with master controller, and master controller is connect by main interface with external signal transducer
Master controller is also connect with input module, output module respectively, and input module is connect with output module, output module and main interface
Connection.The integrated level of device is improved on carrier body by the way that corresponding electrical component to be integrally disposed in, wherein it is preferred that by institute
There is maintenance and operation part that the one side of carrier body is set, is conducive to operation and in time discovery failure and maintenance failure, in addition leads to
It crosses a main interface to connect with complete machine, so that installation and replacement are simple and convenient.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is the embodiments of the present invention, for those of ordinary skill in the art, without creative efforts, also
Other attached drawings can be obtained according to the attached drawing of offer.
Fig. 1 is a kind of knot of aircraft air source truck electrical control gear provided by a kind of specific embodiment of the utility model
Structure schematic diagram；
Fig. 2 is a kind of electricity of aircraft air source truck electrical control gear provided by a kind of specific embodiment of the utility model
The structural schematic diagram of source distribution module；
Fig. 3 is for a kind of aircraft air source truck electrical control gear provided by a kind of specific embodiment of the utility model and outside
The structural schematic diagram of portion's equipment connection.
Appended drawing reference is as follows:
1 is air source truck electrical control gear, and 1.1 be power distribution module, and 1.2 be man-machine interface, and 1.3 be master controller,
1.4 be communication interface, and 1.5 be main interface, and 1.6 be output module, and 1.7 be input module, and 2 be power supply, and 3 be sensing
Device, 4 be engine ECM, and 5 control solenoid valve block for gas source, and 6 be work lamp group, and 7 be program download tool, and 8 be engine diagnostic
Tool, 9 be bus remote control equipment.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-Fig. 3 is please referred to, Fig. 1 is a kind of aircraft air source truck electricity provided by a kind of specific embodiment of the utility model
The structural schematic diagram of gas control device；Fig. 2 is a kind of aircraft air source truck provided by a kind of specific embodiment of the utility model
The structural schematic diagram of the power distribution module of electrical control gear；Fig. 3 is provided by a kind of specific embodiment of the utility model
A kind of structural schematic diagram that is connect with external equipment of aircraft air source truck electrical control gear.
A kind of aircraft air source truck electrical control gear 1 provided by the utility model embodiment, comprising: carrier body and set
Set power distribution module 1.1, man-machine interface 1.2, master controller 1.3, main interface 1.5, input module 1.7 on carrier body
With output module 1.6, main interface 1.5 with power supply 2 for connecting, and wherein the electrical control gear is gone back by main interface 1.5
Information transmitting and control, electricity are carried out with connections such as signal transducer 3, engine ECM4, gas source control solenoid valve 5, work lamp groups 6
Source distribution module 1.1 is used to power to man-machine interface 1.2, master controller 1.3, input module 1.7 and output module 1.6 respectively,
Wherein 1.1 pairs of different equipment of power distribution module are independently controlled and electric current distributes, when overcurrent occurs in corresponding module
When situation, power distribution module 1.1 is protected corresponding, to guarantee not influencing the normal work of other modules, man-machine boundary
Face 1.2 is connect by CAN bus with master controller 1.3, and to realize the transmission of information, man-machine interface 1.2 can be entire blower gas
The electrical system of source vehicle shows operating parameter, fault message and parameter setting etc., and master controller 1.3 is by main interface 1.5 and outside
The signal transducer 3 in portion connects, and handles the information that the external transmission of signal transducer 3 comes, and another part passes through logical process
Directly gas source control solenoid valve block is controlled afterwards, master controller 1.3 also connects with input module 1.7, output module 1.6 respectively
It connects, input module 1.7 is connect with output module 1.6, and output module 1.6 is connect with main interface 1.5, and output module 1.6 receives defeated
Corresponding executing agency is sent to after entering module 1.7 and the control information of master controller 1.3.
In the present embodiment, the integrated of device is improved on carrier body by the way that corresponding electrical component to be integrally disposed in
Degree, wherein it is preferred that all maintenance and operation parts to be arranged in the one side of carrier body, be conducive to operation and in time discovery failure and
Maintenance failure, such as can be by power distribution module 1.1, man-machine interface 1.2, master controller 1.3, input module 1.7 and output mould
The front of carrier body is arranged in block 1.6, and in order to be safeguarded, which refers to that user faces in Operation and maintenance
The one side of user is connect, so that installation and replacement are simple and convenient with complete machine additionally by a main interface 1.5.
Further, be additionally provided with communication interface 1.4 on carrier body, communication interface 1.4 respectively with power distribution module 1.1
It is connected with CAN bus.Communication interface 1.4 and program download tool 7, engine diagnostics tool 8, bus remote control equipment 9 etc. are connect,
Connectivity port is provided for third party's tool and increases the port of additional complete machine bus remote control equipment.Existing communication interface
1.4 be mainly the spare interface that third party's module requires, such as controller needs reserved download port, and engine ECM needs pre-
Hospitalization interruptive port, communication interface 1.4 provided in this embodiment are connect with CAN bus, are had more compared with existing communication interface
Big extension function, it can be achieved that join, reaching can sharing data altogether with the communication cable of entire air source truck electrical control gear 1
It can control the effect of entire control system again.
Specifically, main interface 1.5 is connect with CAN bus.Wherein main interface 1.5 is to be integrated with communication, power supply, input, defeated
The Highgrade integration interface that function is integrated out keeps the communication part of master interface 1.5 and communication interface 1.4 mutually standby
With.
In one embodiment of the utility model, power distribution module 1.1 includes power supply main road and multiple and man-machine boundary
Face 1.2, master controller 1.3, input module 1.7, the power supply of output module 1.6 and main interface 1.5 and communication interface 1.4 1 are a pair of
The power supply branch answered.Wherein power distribution module 1.1 provides power supply main road and power supply branch using recoverable power supply component
Power supply, power supply main road are used for each power supply branch distribution, and each branch of powering does not interfere with each other, and when overcurrent occurs for circuit, are supplied
Electric device can issue alerting signal, such as bright light or instruction device more outstanding than normal condition, to play the mesh of prompting
, and then convenient for being safeguarded in time.
It further, further include monitoring module, monitoring module is used to monitor in real time the use of power supply main road and each power supply branch
Electricity condition and malfunction.It can be understood by monitoring module and know the current working condition of control device.
Further, monitoring module includes alarm module, and alarm module is used for the electricity when power supply main road or branch of powering
Amount issues warning signal when insufficient, and fault-signal is issued when breaking down.User can be reminded to carry out in time by alarm module
Corresponding operation.
Specifically, monitoring module is connect with CAN bus.Monitoring information can be shared with by monitoring module by CAN bus
Entire control device.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.
A kind of aircraft air source truck electrical control gear provided by the utility model is described in detail above.Herein
In apply specific case the principles of the present invention and embodiment be expounded, the explanation of above embodiments is only used
The method and its core concept of the utility model are understood in help.It should be pointed out that for those skilled in the art
For, without departing from the principle of this utility model, several improvements and modifications can be made to this utility model, these
Improvement and modification are also fallen into the protection scope of the utility model claims.
Claims (8)
1. a kind of aircraft air source truck electrical control gear characterized by comprising carrier body and setting are in the carrier body
On power distribution module, man-machine interface, master controller, main interface, input module and output module, the main interface be used for
External main power source connection, the main interface are also connect with the power distribution module, and the power distribution module for giving respectively
The man-machine interface, the master controller, the input module and output module power supply, the man-machine interface pass through CAN bus
It is connect with the master controller, the master controller is connect by the main interface with external signal transducer, the master control
Device processed is also connect with the input module, the output module respectively, and the input module is connect with the output module, described
Output module is connect with the main interface.
2. aircraft air source truck electrical control gear according to claim 1, which is characterized in that also set on the carrier body
There is communication interface, the communication interface is connect with the power distribution module and the CAN bus respectively.
3. aircraft air source truck electrical control gear according to claim 2, which is characterized in that the power distribution module,
The man-machine interface, the master controller, the input module and output module are arranged on the same face of the carrier body.
4. aircraft air source truck electrical control gear according to claim 3, which is characterized in that the main interface with it is described
CAN bus connection.
5. according to the described in any item aircraft air source truck electrical control gears of claim 2 to 4, which is characterized in that the power supply
Distribution module includes that power supply main road and the multiple and man-machine interface, the master controller, the input module, output module supply
The electric and described main interface and the communication interface are powered branch correspondingly.
6. aircraft air source truck electrical control gear according to claim 5, which is characterized in that it further include monitoring module, institute
Monitoring module is stated for monitoring use electricity condition and the malfunction of the power supply main road and each power supply branch in real time.
7. aircraft air source truck electrical control gear according to claim 6, which is characterized in that the monitoring module includes police
Showing module, the alarm module is used to issue warning signal when the not enough power supply when the power supply main road or the power supply branch,
Fault-signal is issued when breaking down.
8. aircraft air source truck electrical control gear according to claim 7, which is characterized in that the monitoring module with it is described
CAN bus connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821443418.XU CN208705701U (en) | 2018-09-03 | 2018-09-03 | A kind of aircraft air source truck electrical control gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821443418.XU CN208705701U (en) | 2018-09-03 | 2018-09-03 | A kind of aircraft air source truck electrical control gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208705701U true CN208705701U (en) | 2019-04-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821443418.XU Expired - Fee Related CN208705701U (en) | 2018-09-03 | 2018-09-03 | A kind of aircraft air source truck electrical control gear |
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| Country | Link |
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| CN (1) | CN208705701U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109062113A (en) * | 2018-09-03 | 2018-12-21 | 山海特种装备股份有限公司 | A kind of aircraft air source truck electrical control gear |
-
2018
- 2018-09-03 CN CN201821443418.XU patent/CN208705701U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109062113A (en) * | 2018-09-03 | 2018-12-21 | 山海特种装备股份有限公司 | A kind of aircraft air source truck electrical control gear |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 410000 No. 1335 Liangtang East Road, Changsha Economic and Technological Development Zone, Hunan Province Patentee after: Shanhe Airport Equipment Co.,Ltd. Address before: 410000 No. 1335 Liangtang East Road, Changsha Economic and Technological Development Zone, Changsha City, Hunan Province Patentee before: SHANHAI SPECIAL EQUIPMENT 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: 20190405 |