CN206892636U - A kind of put-put attaching/detaching apparatus electric control system - Google Patents
A kind of put-put attaching/detaching apparatus electric control system Download PDFInfo
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- CN206892636U CN206892636U CN201720452406.2U CN201720452406U CN206892636U CN 206892636 U CN206892636 U CN 206892636U CN 201720452406 U CN201720452406 U CN 201720452406U CN 206892636 U CN206892636 U CN 206892636U
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Abstract
The utility model provides a kind of put-put attaching/detaching apparatus electric control system, and its mechanical part includes three walking mechanism, elevating mechanism and micro-adjusting mechanism parts, by driving three parts to realize effective dismounting to engine；Electric control system includes programmable logic controller (PLC), communication module, power unit, touch-screen, laser ranging module, pressure sensor, digital video monitoring unit, servo controller, motor, walking mechanism, elevating mechanism and micro-adjusting mechanism.Electric control system uses data processing, servo control and motor drive mode, realizes automatically controlling and being accurately positioned for dismounting engine device；The visual observation of dismounting engine process is realized using digital video monitoring, alleviates manually-operated burden；Change the simple control mode of conventional single-chip microcomputer, improve the antijamming capability of system, improve control system automaticity and reliability, improve operating efficiency, realize intelligent detection and control.
Description
Technical field
The utility model is specifically related to a kind of put-put attaching/detaching apparatus electric control system.
Background technology
Recently as the fast development of aircraft industry, various informative aircraft kind is more and more, baby plane due to
Its small volume, the features such as flexible, price is low, increasingly get more and more people's extensive concerning.Core of the engine as aircraft
Part, in Aircraft Production assembling, the installation and removal work to engine is particularly complicated and important.Domestic Aircraft starts at present
The engine installation car of car, machinery and its hydraulic way is installed in the dismounting of machine using machinery and its engine of hydraulic way mostly
In the presence of automatic degreeization degree it is low, it is cumbersome, waste time and energy, using it is quite inconvenient the problems such as, electronic mode it is actually rare,
And the electrical equipment hardware connection mode that the control system of existing electrodynamic type installation car uses mostly at present, or single-chip microcomputer
Simple control, has that fault rate is high, it is larger to be disturbed, while exists in dismounting engine process and can not operate in real time and visually
A series of problems, such as change observation, can not realize accurate positioning and the control of complicated pose adjustment, and automaticity is not high.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides that a kind of automaticity is high, disassembly efficiency is high, is easy to pair
Connect, posture is easily adjusted, and the baby plane dismounting engine in disassembly process Real Time Observation engine Yu enging cabin gap fills
Put electric control system.
The technical solution of the utility model：
A kind of put-put attaching/detaching apparatus electric control system, the mechanical part of put-put attaching/detaching apparatus include row
Three mechanism, elevating mechanism and micro-adjusting mechanism parts are walked, by driving three parts to realize effective dismounting to engine；
Described electric control system includes programmable logic controller (PLC), communication module, power unit, touch-screen, laser
Range finder module, pressure sensor, digital video monitoring unit, walking servo controller, horizontal fine setting servo controller, longitudinal direction are micro-
Adjust servo controller, course fine setting servo controller, lift servo controller, movable motor, laterally lifting motor, fine setting electricity
Machine, longitudinal direction fine setting motor, course fine setting motor, walking mechanism, elevating mechanism and micro-adjusting mechanism；
Described power unit is connected with programmable logic controller (PLC), touch-screen, digital video monitoring unit respectively, there is provided
Power support, power unit provide the supply of DC24V mains powers for touch-screen and programmable logic controller (PLC), and power unit is number
Word video surveillance unit provides the supply of DC12V mains powers；
Described programmable logic controller (PLC) is connected with touch-screen, laser ranging module, pressure sensor respectively, may be programmed
Logic controller carries out data exchange with touch-screen, on the touchscreen to the motion of walking mechanism, elevating mechanism and micro-adjusting mechanism
Speed and target location are configured, and the running status of system is shown；Programmable logic controller (PLC) is to laser ranging
The output data of module is monitored in real time, ensures that system positions with aircraft position；Pressure sensor gathers engine in real time
Dismounting load, and be transferred to programmable logic controller (PLC), programmable logic controller (PLC) analysis sees if fall out defined limit
Degree；
Described communication module is connected with programmable logic controller (PLC), servo controller, and servo controller is watched including walking
Take controller, laterally lift servo controller, fine setting servo controller, longitudinal direction fine setting servo controller and course fine setting servo control
Device connection processed, programmable logic controller (PLC) transfer data to servo controller by communication module, move its motor；
Walking servo controller is connected with movable motor, and movable motor is connected with walking mechanism, by the operation of movable motor, is realized small
The motion control of h type engine h attaching/detaching apparatus walking mechanism；Lift servo controller is connected with lifting motor, and lifting motor is with rising
Descending mechanism connects, and by transmission data command of the programmable logic controller (PLC) to lift servo controller, drives lifting motor, leads to
The operation of lifting motor is crossed, realizes the driving and control of put-put attaching/detaching apparatus elevating mechanism；Laterally fine setting SERVO CONTROL
Servo controller and longitudinal direction fine setting motor connection, course fine setting servo controller are finely tuned in device and laterally fine setting motor connection, longitudinal direction
Motor connection is finely tuned with course, and laterally fine setting motor, longitudinal direction fine setting motor, course fine setting motor are connected with micro-adjusting mechanism,
By driving laterally fine setting motor, longitudinal motion for finely tuning motor, course fine setting motor, realize to put-put attaching/detaching apparatus
The motion of micro-adjusting mechanism.
Put-put attaching/detaching apparatus electric control system system passes through walking mechanism, upgrading mechanism, the fortune of micro-adjusting mechanism
The dynamic fine motion adjustment for realizing put-put complicated posture during installation and removal, and pass through digital video monitoring unit pair
The gap observation of engine installation and removal, realize system operation and visual observation in real time, accurate positioning and complicated appearance
The Automated condtrol of state adjustment, the movable motor of the control system, laterally lifting motor, fine setting motor, longitudinal direction fine setting motor, boat
Servomotor is used to fine setting motor.
The beneficial effects of the utility model：This electric control system is driven using data processing, servo control and motor
Flowing mode, realize automatically controlling and being accurately positioned for baby plane dismounting engine device；Overcome using digital video monitoring
The conventional deficiencies using the multiple artificial observation installation gaps of tradition, realize the visualization of baby plane dismounting engine process
Observation, alleviates manually-operated burden；Change the simple control mode of conventional single-chip microcomputer, improve the anti-interference energy of system
Power, and improve control system automaticity and reliability, greatly improved operating efficiency, realize intelligent detection and
Control.
Brief description of the drawings
Fig. 1 is a kind of structured flowchart of put-put attaching/detaching apparatus electric control system.
Fig. 2 is a kind of workflow diagram of put-put attaching/detaching apparatus electric control system.
Embodiment
Below in conjunction with accompanying drawing and technical scheme, specific embodiment of the present utility model is further illustrated.
Embodiment
The control system is by programmable logic controller (PLC), communication module, power unit, touch-screen, laser ranging module, pressure
Force snesor, digital video monitoring unit, walking servo controller, lift servo controller, transverse direction are finely tuned servo controller, indulged
To fine setting servo controller, course fine setting servo controller, movable motor, laterally lifting motor, fine setting motor, longitudinal direction fine setting electricity
The composition such as machine, laterally fine setting motor, course fine setting motor, walking mechanism, elevating mechanism, micro-adjusting mechanism group.
Baby plane dismounting engine device includes bottom walking mechanism, the elevating mechanism of center section, walking mechanism with
Elevating mechanism mechanically connects, and is micro-adjusting mechanism on elevating mechanism top, and elevating mechanism mechanically connects with micro-adjusting mechanism, forms small-sized
The integral frame-type mechanical structure of aircraft engine attaching/detaching apparatus.Put-put attaching/detaching apparatus is realized by walking mechanism motion
Walking in a horizontal state, the arrival of specified location can be achieved, the entirety of put-put attaching/detaching apparatus is moved, realized by elevating mechanism
It is raised and lowered, the micro-adjustment of dismounting is realized by micro-adjusting mechanism.Control is sent to programmable logic controller (PLC) by touch-screen
Instruction, and using the motion of servo controller motor, and walking mechanism, elevating mechanism, micro-adjusting mechanism motion are driven, realize small
The automatic installation of type aircraft engine controls with dismounting.
Power unit provides power for system, and two groups of power supplys are exported using battery mode, output DC24V be touch-screen,
Programmable logic controller (PLC) provides power supply, and power unit provides DC12V and provides power supply for digital video monitoring unit.
And power unit is charged using AC220V, power supply supply is carried out, meets actual use demand.
Programmable logic controller (PLC) connects touch-screen, communication module, laser ranging module, pressure sensor respectively.It can compile
Communication interface connection of the journey logic controller equipped with Ethernet interface and touch-screen carries out data exchange and on the right side of controller
Configuration bottom plate is connected with communication module, while extends multiple input/output modules, realizes the collection and control of system.
Touch-screen is responsible for sending movable motor, laterally lifting motor, fine setting motor, longitudinal direction fine setting motor, course fine setting electricity
Main story order, inverted command, the startup of machine are ordered, speed parameter of ceasing and desisting order is set, speed is shown and its status display.Touch
Screen is furnished with ethernet communication interface, is easy to enter row bus with programmable logic controller (PLC) and is connected and the interaction of data, in touch-screen
It is upper to include parameter setting screen respectively, be automatically brought into operation the pictures such as screen, manually operated screen, attended operation screen, status display operator control panel.
System configuration digital video monitoring unit, video surveillance unit is by camera, monitor, display screen three parts group
Into.Video monitoring is carried out to the disassembly process of aircraft using camera, installed in the multiple assistant windows of aircraft inner chamber body flank
Fine definition minisize pick-up head, by monitor handle video, and by display screen observe engine installation and removal process,
Gap between observation engine gabarit and aircaft configuration frame in real time, avoids engine gabarit from being touched with aircaft configuration frame
Hit.
Communication module is arranged on the right side of programmable logic controller (PLC), is connect by the RS485+ on communication module and RS485-
Line terminals with walking servo controller, lift servo controller, laterally fine setting servo controller, longitudinal direction fine setting servo controller,
Course fine setting servo controller connection, communication module have MODBUS-RTU communications protocol, while the number that communication module is gathered
Analyzed and handled according to programmable functions logic controller is transferred to.
Laser range sensor is connected with Programmable logical controller, installed in the front portion of micro-adjusting mechanism, passes through laser ranging
Sensor carries out the positioning of dismounting engine system and aircraft relative position.Laser range sensor sends a branch of red during work
Laser, it is incident upon on target plate and forms red point, and then measures relative distance and send measurement number to programmable logic controller (PLC) in real time
According to being positioned, while data will be fed back in touch screen interface, facilitate staff to check, laser range sensor coverage
For 200mm to 2000mm.
Pressure sensor is connected with Programmable logical controller, and pressure sensor is installed on micro-adjusting mechanism, to the pressure of support
Power is detected in real time, and is transmitted a signal to programmable logic controller (PLC) and handled.When pressure reaches pressure set in advance
During force value, system carries out alarm.Ensure that load unloads in advance during dismounting engine, prevents the engine in disassembling and assembling engine
Thrust pin sustains damage.
Walking servo controller is connected with movable motor, and movable motor is connected with walking mechanism, utilizes FPGA control
The movement instruction that device processed is sent, movable motor are controlled motion, realize the motion control of put-put dismounting walking mechanism；
Lift servo controller is connected with lifting motor, and lifting motor is connected with elevating mechanism, by programmable logic controller (PLC) to rising
The transmission data command of servo controller is dropped, drives lifting motor, by the operation of lifting motor, realizes that put-put dismounts
The driving and control of elevating mechanism；Laterally fine setting servo controller finely tunes servo controller with laterally fine setting motor connection, longitudinal direction
With longitudinal direction fine setting motor connection, course fine setting servo controller and course fine setting motor connection, and will laterally finely tune motor, longitudinal direction
Fine setting motor, course fine setting motor are connected with micro-adjusting mechanism, and by driving, laterally fine setting motor, longitudinal direction fine setting motor, course are micro-
The motion of motor is adjusted, realizes the motion of baby plane dismounting engine micro-adjusting mechanism.
Operating personnel are used by operating instruction when control system works, and working-flow is referring to accompanying drawing 2, and connection power supply is just
Often after work, sending control instruction by touch-screen runs walking mechanism, and is detected using laser range sensor and carry out phase
Positioning to position, after positioning is completed, control instruction is sent by touch-screen and drives elevating mechanism to run, reaches specified location
Afterwards, the support pressure for micro-adjusting mechanism being detected using pressure sensor is detected in real time, after alarm free, then is sent by touch-screen
Control instruction driving micro-adjusting mechanism operation, during being adjusted to micro-adjusting mechanism, while utilize digital video observation dismounting gap
Collision situation, after fine motion adjustment ensures the intact docking of engine, stop adjustment, complete the whole mistake of baby plane dismounting engine
Journey, realize the efficient installation of engine.
Claims (1)
- A kind of 1. put-put attaching/detaching apparatus electric control system, it is characterised in that the machinery of put-put attaching/detaching apparatus Part includes three walking mechanism, elevating mechanism and micro-adjusting mechanism parts, by driving three parts to realize have to engine Effect dismounting；Described electric control system includes programmable logic controller (PLC), communication module, power unit, touch-screen, laser ranging Module, pressure sensor, digital video monitoring unit, walking servo controller, horizontal fine setting servo controller, longitudinal direction fine setting are watched Take controller, servo controller is finely tuned in course, lift servo controller, movable motor, lifting motor, transverse direction finely tune motor, vertical To fine setting motor, course fine setting motor, walking mechanism, elevating mechanism and micro-adjusting mechanism；Described power unit is connected with programmable logic controller (PLC), touch-screen, digital video monitoring unit respectively, there is provided power Support, power unit provides the supply of DC24V mains powers for touch-screen and programmable logic controller (PLC), and power unit regards for numeral Frequency monitoring unit provides the supply of DC12V mains powers；Described programmable logic controller (PLC) is connected with touch-screen, laser ranging module, pressure sensor respectively, FPGA Controller carries out data exchange with touch-screen, on the touchscreen to the movement velocity of walking mechanism, elevating mechanism and micro-adjusting mechanism It is configured with target location, and the running status of system is shown；Programmable logic controller (PLC) is to laser ranging module Output data monitored in real time, ensure that system and aircraft position position；Pressure sensor gathers tearing open for engine in real time Lotus is loaded, and is transferred to programmable logic controller (PLC), programmable logic controller (PLC) analysis sees if fall out defined limit；Described communication module is connected with programmable logic controller (PLC), servo controller, and servo controller includes walking servo control Device, lift servo controller, horizontal fine setting servo controller, longitudinal direction fine setting servo controller and course fine setting servo controller processed Connection, programmable logic controller (PLC) transfer data to servo controller by communication module, move its motor；Walking Servo controller is connected with movable motor, and movable motor is connected with walking mechanism, by the operation of movable motor, realizes small-sized hair The motion control of motivation attaching/detaching apparatus walking mechanism；Lift servo controller is connected with lifting motor, lifting motor and lift Structure connects, and by transmission data command of the programmable logic controller (PLC) to lift servo controller, drives lifting motor, passes through liter The operation of motor is dropped, realizes the driving and control of put-put attaching/detaching apparatus elevating mechanism；Laterally fine setting servo controller with Servo controller and longitudinal direction fine setting motor connection, course fine setting servo controller and boat are finely tuned in laterally fine setting motor connection, longitudinal direction It is connected, passes through with micro-adjusting mechanism to fine setting motor connection, and by laterally fine setting motor, longitudinal direction fine setting motor, course fine setting motor Driving laterally fine setting motor, longitudinal motion for finely tuning motor, course fine setting motor, realizes and put-put attaching/detaching apparatus is finely tuned The motion of mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720452406.2U CN206892636U (en) | 2017-04-27 | 2017-04-27 | A kind of put-put attaching/detaching apparatus electric control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720452406.2U CN206892636U (en) | 2017-04-27 | 2017-04-27 | A kind of put-put attaching/detaching apparatus electric control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206892636U true CN206892636U (en) | 2018-01-16 |
Family
ID=61324879
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720452406.2U Withdrawn - After Issue CN206892636U (en) | 2017-04-27 | 2017-04-27 | A kind of put-put attaching/detaching apparatus electric control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206892636U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106933181A (en) * | 2017-04-27 | 2017-07-07 | 沈阳飞机工业（集团）有限公司 | A kind of put-put attaching/detaching apparatus electric control system |
-
2017
- 2017-04-27 CN CN201720452406.2U patent/CN206892636U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106933181A (en) * | 2017-04-27 | 2017-07-07 | 沈阳飞机工业（集团）有限公司 | A kind of put-put attaching/detaching apparatus electric control system |
| CN106933181B (en) * | 2017-04-27 | 2023-07-18 | 沈阳飞机工业（集团）有限公司 | Electrical control system of small-sized engine dismounting device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20180116 Effective date of abandoning: 20230718 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20180116 Effective date of abandoning: 20230718 |