CN204753686U - Automatically controlled guide control system redundancy apparatus of excavator - Google Patents
Automatically controlled guide control system redundancy apparatus of excavator Download PDFInfo
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- CN204753686U CN204753686U CN201520101777.7U CN201520101777U CN204753686U CN 204753686 U CN204753686 U CN 204753686U CN 201520101777 U CN201520101777 U CN 201520101777U CN 204753686 U CN204753686 U CN 204753686U
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- automatically controlled
- control valve
- pilot control
- excavator
- valve group
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Abstract
The utility model discloses an automatically controlled guide control system redundancy apparatus of excavator, which comprises a controller, automatically controlled guide handles the valves, electromagnetic switch valves and electromagnetism proportion valves, automatically controlled guide handles the valves and passes through CAN bus no. 1 and controller electricity and be connected, electromagnetic switch valves and electromagnetism proportion valves are connected with the controller electricity, still including the display that is used for showing automatically controlled pilot system emergency maneuver interface, the display passes through CAN bus no. 2 and is connected with the controller electricity, automatically controlled pilot system emergency maneuver interface is including being used for controlling automatically controlled guide's operating valve composition marking to the action, and be used for realizing that automatically controlled guide handles the valves circulation and switches over, carry out automatically controlled guide's operating valve composition to action and function cancellation function button. The utility model discloses utilize excavator self to have the configuration, carry out the emergence operation to automatically controlled guide control system through the display, promoted the automatically controlled control system's of excavator reliability and the security that the excavator used.
Description
Technical field
The utility model relates to a kind of excavator redundant apparatus, and specifically the automatically controlled precursor operation system redundant apparatus of a kind of excavator, belongs to excavator electronic control technology field.
Background technology
Current excavator precursor operation system generally controls main control valves by two control cranks and two are foot-operated, then by the action of main control valve hydraulic control oil cylinder and hydraulic motor.Large-sized mining dredger be raising system response speed, simplify fluid pressure line and electric wiring, the automatically controlled guide's driven valve of reduction cost of production many employings CAN.Received the signal of automatically controlled pilot control valve by controller, and drive electromagnetic switch valve and electromagnetic proportional valve to control main control valve, then control excavator action by main control valve.
When control crank break down or CAN Communications failure time, the action of excavator is by uncontrolled, very large obstacle is brought to the use of excavator, if excavator cannot telephone-moving to need the occasion of explosion to occur at some, huge potential safety hazard can be caused, or excavator breaks down on important transportation passage, also huge economic loss can be brought for producing.
Summary of the invention
For above-mentioned prior art Problems existing, the automatically controlled precursor operation system redundant apparatus of a kind of excavator of the purpose of this utility model, solve the problem that pilot control valve fault or bus communication unsuccessfully cause machine to work, make full use of the existing configuration of excavator, when not increasing complete machine cost, improve the reliability of excavator electric control manipulation system and the safety of excavator use.
To achieve these goals, the utility model provides the automatically controlled precursor operation system redundant apparatus of a kind of excavator, comprise controller, automatically controlled pilot control valve group, electromagnetic switch valve group and electromagnetic proportional valve group, described automatically controlled pilot control valve group is electrically connected with controller by CAN one, described electromagnetic switch valve group and electromagnetic proportional valve group are electrically connected with controller, also comprise the display for showing automatically controlled pilot system emergency maneuver interface, described display is electrically connected with controller by CAN two, described automatically controlled pilot system emergency maneuver interface comprises for controlling the sign of automatically controlled pilot control valve prescription to action, and for realizing automatically controlled pilot control valve group cyclic switching, perform automatically controlled pilot control valve prescription and cancel function button to action and function.
Preferably, described automatically controlled pilot control valve group comprises right foot pedal, left and right walking bi-pedal, left foot pedal, right handles and left handle, and described function button is F1, F2, F3, F4, F5 and F6;
Described left and right handle has X+, X-, Y+, Y-four-way operating function, and left and right foot pedal has Y+, Y-bidirectional operation function;
Described function button F1 is defined as cyclic switching button; Function button F2 is defined as and performs pilot control valve X+ direction action key, function button F3 is defined as and performs pilot control valve Y+ direction action key, function button F4 is defined as and performs pilot control valve Y-direction action key, function button F5 is defined as and performs pilot control valve X-direction action key, and function button F6 is defined as function and cancels button.
Preferably, display is divided into viewing area and non-display area, described left and right handle, left and right foot pedal, and the sign of left and right walking bi-pedal shows in the display area, and described function button F1 ~ F6 is arranged on non-display area.
Preferably, display is touch screen displays.
Preferably, the electromagnetic switch valve group output voltage that described controller controls is 24V.
Preferably, the electromagnetic proportional valve group output signal that controller controls is PWM.
Compared with prior art, the utility model is when automatically controlled precursor operation system normally works, and controller receives first automatically controlled pilot control valve signal, exports relevant voltage and PWM, realizes the normal work of electronic control system of excavator.When there is Communications failure in a certain automatically controlled pilot control valve fault, multiple automatically controlled pilot control valve fault or the CAN between controller and automatically controlled pilot control valve, the function of corresponding control crank can be realized by display automatically controlled guide emergency maneuver interface, ensure that the elemental motion of excavator.
The utility model utilizes the existing configuration of excavator self, by display, emergency operation is carried out to automatically controlled precursor operation system, improve the reliability of excavator electric control manipulation system and the safety of excavator use in the mode of relatively low cost, simple, intuitive.
Accompanying drawing explanation
Fig. 1 is principle schematic of the present utility model;
Fig. 2 is the electric control schematic diagram of the utility model embodiment;
Fig. 3 is pilot control valve direction of motion schematic diagram;
Fig. 4 is the man-machine interface of the utility model embodiment.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1 and Figure 4, the automatically controlled precursor operation system redundant apparatus of a kind of excavator, comprise controller, automatically controlled pilot control valve group, electromagnetic switch valve group, electromagnetic proportional valve group and the display for showing automatically controlled pilot system emergency maneuver interface, described electromagnetic switch valve group and electromagnetic proportional valve group are electrically connected with controller, and described controller carries out communication by CAN one and automatically controlled pilot control valve group; Described display carries out communication by CAN two and controller; Controller, according to collecting automatically controlled pilot control spool parameter after calculating, exports+24V and controls electromagnetic switch valve group, exports and controls electromagnetic proportional valve group with the pwm signal of automatically controlled pilot control valve proportion of composing.
Described automatically controlled pilot system emergency maneuver interface comprises for controlling the sign of automatically controlled pilot control valve prescription to action, and for realizing automatically controlled pilot control valve group cyclic switching, performing automatically controlled pilot control valve prescription to action and function cancellation function button.Described display, for showing pilot valve mode of operation, carries out emergency operation to automatically controlled precursor operation system simultaneously.
As shown in Figure 2, described automatically controlled pilot control valve group comprises right foot pedal, left and right walking bi-pedal, left foot pedal, right handles and left handle, and each automatically controlled pilot control valve is for controlling excavator corresponding main control valve spool pilot pressure.
As shown in Figure 3, described left and right handle has X+, X-, Y+, Y-four-way operating function, and left and right foot pedal has Y+, Y-bidirectional operation function.
As shown in Figure 4, described display is divided into viewing area and non-display area, described left and right handle, left and right foot pedal, the sign of left and right walking bi-pedal shows in the display area, and described function button comprises F1, F2, F3, F4, F5 and F6, and is arranged on non-display area.Viewing area is according to from left to right (being " left side " on the left of Fig. 1, right side is for " right side ") order be defined as that left handle indicates, right handles indicates, left threading indicates, left and right bi-pedal indicates and right threading sign successively, each sign only has an energy selected, indicate selected after, with solid border with do not choose sign to distinguish, and carry out cyclic switching by function button F1; Function button F2 is defined as and performs pilot control valve X+ direction action key, function button F3 is defined as and performs pilot control valve Y+ direction action key, function button F4 is defined as and performs pilot control valve Y-direction action key, and function button F5 is defined as and performs pilot control valve X-direction action key.Left handle or right handles indicate selected after, function button F2 ~ F5 button all can be triggered, and left threading, left and right bi-pedal or right threading indicate selected rear function button F3, F4 button and can be triggered, and function button F6 is defined as function and cancels button.
Certainly also can be touch screen displays, each automatically controlled pilot control valve indicates and function button F1 ~ F6 all shows in touch screen displays, operates more convenient.
The course of work: controller receives automatically controlled pilot control valve group signal, and output switching signal, pwm signal control corresponding electromagnetic switch valve and electromagnetic proportional valve after computing, thus control excavator action.Under excavator is in non-faulting state, driver handles corresponding automatically controlled pilot control valve according to action demand, direction and the manipulation scaling signal of automatically controlled pilot control valve are delivered to controller by CAN one, controller exports+24V and electrically connects corresponding electromagnetic switch valve, output pwm signal triggering electromagnetic proportional valve, the function of the pilot control valve corresponding to excavator performs, by CAN two, automatically controlled pilot control valve signal is delivered on display with Time Controller, the display of display man-machine interface is by pilot valve, steering and the manipulation ratio handled.If a certain control crank breaks down, multiple handle break down or CAN one Communications failure time, controller judges automatically controlled pilot control valve device fault, and send instruction activation display electric control handle emergency maneuver man-machine interface by CAN two, in man-machine interface, definition represents the automatically controlled pilot control valve of difference in functionality, each automatically controlled pilot control valve mark carries out cyclic switching by the function button of definition, and ensure to only have a control crank selected, driver can according to equipment fault situation and action demand, length pins watch-dog directionkeys up and down, push button signalling is transferred to controller by CAN two by watch-dog, thus have activated the function of control crank corresponding to it.
In excavator manipulation of physical, breaking down for left handle, the utility model is described in further detail.
The left revolution of the corresponding excavator in the X+ direction of left handle, the corresponding excavator right-hand rotation in X-direction, the corresponding excavator boom in Y+ direction are put outward, the corresponding excavator boom adduction in Y-direction, controller carries out scan round with the fixed cycle to CAN one, if left handle breaks down, then controller cannot receive the control signal of left handle, if now driver wishes that handling left handle carries out turning round or dipper action, excavator is without response.Controller still cannot receive CAN one data of left handle after multiple intermittent scanning, then judge left handle generation equipment fault, and send instructions to display by CAN two, display activates automatically controlled pilot system emergency maneuver interface.Driver chooses left handle to indicate by function button F1, this duration pins F2 key, the signal that left handle X+ direction is triggered is transferred to controller by CAN two by display, controller exports+24V to left revolution electromagnetic switch valve 301, export a fixing pwm signal to left revolution electromagnetic proportional valve 501, excavator performs left revolution, and after function button F2 upsprings, left revolution stops.If pin equally F5 key excavator to carry out right-hand rotation, pin F3 key excavator boom and put outward, pin F4 key excavator boom adduction.
If when right foot pedal, left foot pedal, right handles CAN one break down, of the present utility modelly realize principle, method of operating breaks down consistent with left handle.
Claims (6)
1. the automatically controlled precursor operation system redundant apparatus of excavator, comprise controller, automatically controlled pilot control valve group, electromagnetic switch valve group and electromagnetic proportional valve group, described automatically controlled pilot control valve group is electrically connected with controller by CAN one, described electromagnetic switch valve group and electromagnetic proportional valve group are electrically connected with controller, it is characterized in that, also comprise the display for showing automatically controlled pilot system emergency maneuver interface, described display is electrically connected with controller by CAN two, described automatically controlled pilot system emergency maneuver interface comprises for controlling the sign of automatically controlled pilot control valve prescription to action, and for realizing automatically controlled pilot control valve group cyclic switching, perform automatically controlled pilot control valve prescription and cancel function button to action and function.
2. the automatically controlled precursor operation system redundant apparatus of a kind of excavator according to claim 1, it is characterized in that, described automatically controlled pilot control valve group comprises right foot pedal, left and right walking bi-pedal, left foot pedal, right handles and left handle, and described function button is F1, F2, F3, F4, F5 and F6;
Described left and right handle has X+, X-, Y+, Y-four-way operating function, and left and right foot pedal has Y+, Y-bidirectional operation function;
Described function button F1 is defined as cyclic switching button; Function button F2 is defined as and performs pilot control valve X+ direction action key, function button F3 is defined as and performs pilot control valve Y+ direction action key, function button F4 is defined as and performs pilot control valve Y-direction action key, function button F5 is defined as and performs pilot control valve X-direction action key, and function button F6 is defined as function and cancels button.
3. the automatically controlled precursor operation system redundant apparatus of a kind of excavator according to claim 1 and 2, it is characterized in that, described display is divided into viewing area and non-display area, described left and right handle, left and right foot pedal, left and right being indicated in viewing area of bi-pedal of walking shows, and described function button F1 ~ F6 is arranged on non-display area.
4. the automatically controlled precursor operation system redundant apparatus of a kind of excavator according to claim 1 and 2, is characterized in that, described display is touch screen displays.
5. the automatically controlled precursor operation system redundant apparatus of a kind of excavator according to claim 4, is characterized in that, the electromagnetic switch valve group output voltage that described controller controls is 24V.
6. the automatically controlled precursor operation system redundant apparatus of a kind of excavator according to claim 5, is characterized in that, the electromagnetic proportional valve group output signal that described controller controls is PWM.
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105892716A (en) * | 2016-05-04 | 2016-08-24 | 刘其锋 | Keyboard redundant method and structure based on multiple keys in same region |
CN109750715A (en) * | 2017-11-06 | 2019-05-14 | 罗伯特·博世有限公司 | Device and method for controlling Work machine |
CN113062377A (en) * | 2021-03-31 | 2021-07-02 | 上海三一重机股份有限公司 | Positive and negative hand switching method and system for electric control excavator, electronic equipment and storage medium |
CN114250821A (en) * | 2021-12-28 | 2022-03-29 | 徐州徐工挖掘机械有限公司 | Excavator emergency operation control system and method |
CN114775723A (en) * | 2022-05-24 | 2022-07-22 | 江苏朗禾控制系统有限公司 | Intelligent electric control handle for excavator |
CN115233765A (en) * | 2022-08-19 | 2022-10-25 | 徐州徐工挖掘机械有限公司 | Emergency operation control method and device |
-
2015
- 2015-02-12 CN CN201520101777.7U patent/CN204753686U/en active Active
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105892716A (en) * | 2016-05-04 | 2016-08-24 | 刘其锋 | Keyboard redundant method and structure based on multiple keys in same region |
CN105892716B (en) * | 2016-05-04 | 2019-04-30 | 刘其锋 | Keyboard redundancy approach and structure based on the multiple key of same area |
CN109750715A (en) * | 2017-11-06 | 2019-05-14 | 罗伯特·博世有限公司 | Device and method for controlling Work machine |
CN113062377A (en) * | 2021-03-31 | 2021-07-02 | 上海三一重机股份有限公司 | Positive and negative hand switching method and system for electric control excavator, electronic equipment and storage medium |
CN114250821A (en) * | 2021-12-28 | 2022-03-29 | 徐州徐工挖掘机械有限公司 | Excavator emergency operation control system and method |
CN114775723A (en) * | 2022-05-24 | 2022-07-22 | 江苏朗禾控制系统有限公司 | Intelligent electric control handle for excavator |
CN115233765A (en) * | 2022-08-19 | 2022-10-25 | 徐州徐工挖掘机械有限公司 | Emergency operation control method and device |
CN115233765B (en) * | 2022-08-19 | 2024-02-27 | 徐州徐工挖掘机械有限公司 | Emergency operation control method and device |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right |
Effective date of registration: 20180427 Address after: 221000 39 Gaoxin Road, Xuzhou economic and Technological Development Zone, Xuzhou, Jiangsu Patentee after: Xuzhou Xugong Mining Machinery Co., Ltd. Address before: 221000 39 Gaoxin Road, Xuzhou Economic Development Zone, Jiangsu Patentee before: XCMG Excavator Machinery Co., Ltd. |
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TR01 | Transfer of patent right |