CN205158019U - Laser leveling machine's landing leg automatic balance control system - Google Patents

Laser leveling machine's landing leg automatic balance control system Download PDF

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Publication number
CN205158019U
CN205158019U CN201520830900.9U CN201520830900U CN205158019U CN 205158019 U CN205158019 U CN 205158019U CN 201520830900 U CN201520830900 U CN 201520830900U CN 205158019 U CN205158019 U CN 205158019U
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CN
China
Prior art keywords
supporting leg
controller
solenoid valve
module
landing leg
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Expired - Fee Related
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CN201520830900.9U
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Chinese (zh)
Inventor
张长江
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Xugong Chongqing Engineering Machinery Co Ltd
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Xugong Chongqing Engineering Machinery Co Ltd
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Priority to CN201520830900.9U priority Critical patent/CN205158019U/en
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Expired - Fee Related legal-status Critical Current
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Abstract

The utility model discloses a laser leveling machine's landing leg automatic balance control system, including landing leg control module, pressure sensor module, controller, landing leg solenoid valve module, biax angular transducer, display, wherein landing leg control module links to each other with the switching value input of controller, pressure sensor module links to each other with the analog input end of controller for detect landing leg lift cylinder's pressure, landing leg solenoid valve module links to each other with the switched output end of controller for control the lift of the flexible of landing leg lift cylinder and then control landing leg, biax angular transducer links to each other with the CAN bus in end of controller for detect the levelness of fuselage X axle and Y axle, the display links to each other with the CAN bus out end of controller for the levelness that shows fuselage X axle and Y axle. The mode of leveling artifical manual relatively, the utility model discloses a full auto leveling control has not only improved efficiency, and leveling result moreover is more accurate reliable, has guaranteed whole operating mass with rated load.

Description

A kind of supporting leg automatic balance control system of laser leveling machine
Technical field
The utility model relates to a kind of supporting leg automatic balance control system of laser leveling machine.
Background technology
Large laser bump-cutter machine is because of need of work, must ensure that car load is in horizontality, the form that supporting structure adopts four supporting legs to support usually, supporting leg controls lifting by hydraulic jack respectively, the hydraulic valve of support oil cylinder is controlled by manual handles, realize the flexible of oil cylinder, and then control, horizontality that the lifting of supporting leg adjusted realizes car load, and judge fuselage whether leveling by observing the level meter of fuselage, but level meter can only determine the level condition in a direction, cannot reflect whether complete machine is up to the standard state.The each operation bout of bump-cutter machine needs to readjust car load horizontality, this manual shift mode regulates inconvenience, error is large, generally about about 1 minute consuming time, and the time of average next operation bout every of common bump-cutter machine is also only 3 minutes, thus manual leveling reduces overall operating efficiency to heavens.
Utility model content
For the problems referred to above of the prior art, the utility model proposes a kind of supporting leg automatic balance control system of laser leveling machine, can realize realizing automatically, accurately controlling to the supporting leg of laser leveling machine, thus the balance realizing fuselage controls.
The technical solution of the utility model is: a kind of supporting leg automatic balance control system of laser leveling machine, comprises supporting leg control module, pressure sensor module, controller, supporting leg solenoid valve module, double-shaft tilt angle sensor, wherein:
Described supporting leg control module comprises supporting leg raise button, supporting leg decline leveling button, described supporting leg raise button, supporting leg decline leveling button are connected with the On-off signal end of controller respectively, and described supporting leg control module is used for manual control signal to be transferred to controller;
Described pressure sensor module is connected with the analog input end of controller, for detecting the pressure of supporting leg hoist cylinder and pressure signal being transferred to controller;
Described supporting leg solenoid valve module is connected with the output switching terminal of controller, for receiving the control signal of controller and controlling the flexible of supporting leg hoist cylinder and then control the lifting of supporting leg;
Described double-shaft tilt angle sensor is connected with the CAN input end of controller, for detecting the levelness of fuselage X-axis and Y-axis in real time and detection data being transferred to controller;
Described controller is used for the signal imported into of supporting leg control module, pressure sensor module and double-shaft tilt angle sensor and data analysis, process, and switch controlling signal is outputted to supporting leg solenoid valve module.
Further, the display be connected with the CAN output terminal of controller is also comprised, for showing the levelness of fuselage X-axis and Y-axis.
Further, described supporting leg control module also comprises the supporting leg A independence gauge tap, legs B independence gauge tap, supporting leg C independence gauge tap, the supporting leg D independence gauge tap that are connected with the On-off signal end of controller respectively; Pressure sensor module comprises the supporting leg A pressure transducer, legs B pressure transducer, supporting leg C pressure sensor, the supporting leg D pressure transducer that are connected with the analog input end of controller respectively; Described supporting leg solenoid valve module comprises the supporting leg A solenoid valve, legs B solenoid valve, supporting leg C solenoid valve, the supporting leg D solenoid valve that are connected with the output switch parameter end of controller respectively.
Principle of work of the present utility model is: by pressure sensor module detection supporting leg hoist cylinder pressure and by pressure signal transmission to controller, and whether all controller contrasts the Pressure Analysis of each supporting leg hoist cylinder and then judge each supporting leg kiss the earth; Then detect the levelness of fuselage by double-shaft tilt angle sensor and levelness data are delivered to controller, controller is analyzed levelness and then is judged whether fuselage is in level, if out-of-level, control supporting leg lifting by supporting leg solenoid valve module, thus leveling fuselage; Meanwhile, standard of fuselage degree is shown by display, and operator also carries out manual leveling by supporting leg control module.
Compared with prior art, the beneficial effects of the utility model are:
1. the utility model detects the X-axis of horizontal direction and the levelness of Y-axis in real time by being arranged on the double-shaft tilt angle sensor on fuselage, leveling is carried out again according to detection data, with in prior art by compared with manual observation level meter, testing result of the present utility model is more accurate, thus leveling result is also more accurate, and then ensure that the quality of leveling work;
2. the utility model controls by controller the control that supporting leg solenoid valve module realizes supporting leg, and then achieve full-automatic leveling, and automatic leveling controls consuming timely to be only about 10 seconds, by the mode of artificial leveling in hinge structure, the utility model drastically increases work efficiency, indirectly creates huge economic benefit;
3. the utility model detects by adopting the pressure of pressure sensor module to supporting leg hoist cylinder, thus judge whether supporting leg lands completely, avoid and occur standard of fuselage but the situation still having supporting leg unsettled, make fuselage more firm, ensure that fuselage there will not be the situation of toppling when the work of leveling, avoids and occurs security incident;
4. the utility model is by arranging supporting leg independence gauge tap, adds the function of artificial leveling, makes product function more perfect.
Accompanying drawing explanation
Fig. 1 is system architecture diagram of the present utility model.
Wherein: 1-supporting leg control module, 2-pressure sensor module, 3-controller, 4-supporting leg solenoid valve module, 5-double-shaft tilt angle sensor, 6-display.
Embodiment
Below in conjunction with drawings and Examples, the technical scheme in the utility model is further illustrated.
As shown in Figure 1, the utility model comprises supporting leg control module 1, pressure sensor module 2, controller 3, supporting leg solenoid valve module 4, double-shaft tilt angle sensor 5, display 6, wherein:
Described supporting leg control module 1 is connected with the On-off signal end of controller 3, controller 3 is transferred to for by manual control signal, and described supporting leg control module 1 comprises supporting leg raise button, supporting leg decline leveling button, supporting leg A independence gauge tap, legs B independence gauge tap, supporting leg C independence gauge tap and supporting leg D independence gauge tap, wherein said supporting leg raise button, supporting leg decline leveling button is used for controlling the lifting of four supporting legs is unified, described supporting leg A independence gauge tap, legs B independence gauge tap, supporting leg C independence gauge tap and supporting leg D independence gauge tap are used for the lifting controlling wherein each supporting leg respectively,
Described pressure sensor module 2 is connected with the analog input end of controller 3, pressure signal is transferred to controller 3 for the pressure detecting supporting leg hoist cylinder, and described pressure sensor module 2 comprises supporting leg A pressure transducer, legs B pressure transducer, supporting leg C pressure sensor, supporting leg D pressure transducer;
Described supporting leg solenoid valve module 4 is connected with the output switching terminal of controller 3, for receiving the control signal of controller 3 and controlling the flexible of supporting leg hoist cylinder and then control the lifting of supporting leg, and described supporting leg solenoid valve module 4 comprises supporting leg A solenoid valve, legs B solenoid valve, supporting leg C solenoid valve, supporting leg D solenoid valve;
Described double-shaft tilt angle sensor 5 is connected with the CAN input end of controller 3, for detecting the levelness of fuselage X-axis and Y-axis in real time and detection data being transferred to controller 3;
Described display 6 is connected with the CAN output terminal of controller 3, for showing the levelness of fuselage X-axis and Y-axis;
Described controller 3 is analyzed for the data imported into supporting leg control module 1, pressure sensor module 2 and double-shaft tilt angle sensor 5 and signal, is processed, and control signal is outputted to supporting leg solenoid valve module 4, and vision signal is outputted to display 6.
The present embodiment is to have the bump-cutter machine of four supporting legs, the leveling course of work is: after first bump-cutter machine drives to appointed place, stretched out by supporting leg decline leveling button control four supporting legs simultaneously, pressure sensor module 2 detects the pressure of each supporting leg hoist cylinder simultaneously, and analyzed by controller 3 pairs of pressure signals, when the pressure of four supporting leg hoist cylinders reaches predetermined value, then control four supporting legs and stretch out a period of time simultaneously and make wheel completely liftoff; The levelness data analysis that last controller 3 pairs of double-shaft tilt angle sensors 5 input, when judge fuselage which point be in low level time, stretch out with regard to the supporting leg which point controls, when 4 are highly identical, namely represent that fuselage is up to the standard, and then terminate leveling and lock supporting leg.The utility model achieves full-automatic leveling and controls, and adopt the mode of leveling manually in hinge structure, the utility model not only efficiency greatly improves, and leveling result more accurately and reliably, ensure that the overall work quality of bump-cutter machine.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.

Claims (3)

1. the supporting leg automatic balance control system of a laser leveling machine, it is characterized in that, comprise supporting leg control module (1), pressure sensor module (2), controller (3), supporting leg solenoid valve module (4), double-shaft tilt angle sensor (5), wherein:
Described supporting leg control module (1) comprises supporting leg raise button, supporting leg decline leveling button, described supporting leg raise button, supporting leg decline leveling button are connected with the On-off signal end of controller (3) respectively, and described supporting leg control module (1) is for being transferred to controller (3) by manual control signal;
Described pressure sensor module (2) is connected with the analog input end of controller (3), for detecting the pressure of supporting leg hoist cylinder and pressure signal being transferred to controller (3);
Described supporting leg solenoid valve module (4) is connected with the output switching terminal of controller (3), for receiving the control signal of controller (3) and controlling the flexible of supporting leg hoist cylinder and then control the lifting of supporting leg;
Described double-shaft tilt angle sensor (5) is connected with the CAN input end of controller (3), for detecting the levelness of fuselage X-axis and Y-axis in real time and detection data being transferred to controller (3);
Switch controlling signal for the signal imported into of supporting leg control module (1), pressure sensor module (2) and double-shaft tilt angle sensor (5) and data analysis, process, and is outputted to supporting leg solenoid valve module (4) by described controller (3).
2. the supporting leg automatic balance control system of a kind of laser leveling machine as claimed in claim 1, it is characterized in that: also comprise the display (6) be connected with the CAN output terminal of controller (3), for showing the levelness of fuselage X-axis and Y-axis.
3. the supporting leg automatic balance control system of a kind of laser leveling machine as claimed in claim 1, is characterized in that: described supporting leg control module (1) also comprises the supporting leg A independence gauge tap, legs B independence gauge tap, supporting leg C independence gauge tap, the supporting leg D independence gauge tap that are connected with the On-off signal end of controller (3) respectively; Pressure sensor module (2) comprises the supporting leg A pressure transducer, legs B pressure transducer, supporting leg C pressure sensor, the supporting leg D pressure transducer that are connected with the analog input end of controller (3) respectively; Described supporting leg solenoid valve module (4) comprises the supporting leg A solenoid valve, legs B solenoid valve, supporting leg C solenoid valve, the supporting leg D solenoid valve that are connected with the output switch parameter end of controller (3) respectively.
CN201520830900.9U 2015-10-23 2015-10-23 Laser leveling machine's landing leg automatic balance control system Expired - Fee Related CN205158019U (en)

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Application Number Priority Date Filing Date Title
CN201520830900.9U CN205158019U (en) 2015-10-23 2015-10-23 Laser leveling machine's landing leg automatic balance control system

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CN205158019U true CN205158019U (en) 2016-04-13

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107246848A (en) * 2017-04-21 2017-10-13 江西省高速公路投资集团有限责任公司 A kind of constructing tunnel fracture morphology rapid detection system and its detection method
CN107352250A (en) * 2017-07-05 2017-11-17 宁夏天地奔牛实业集团有限公司 Self-leveling type belt self-movable foot end and belt self-movable foot end self-leveling method
CN108829041A (en) * 2018-07-13 2018-11-16 安徽工程大学 A kind of numerically-controlled machine tool multi-axis controller of self-stabilization
CN110515397A (en) * 2019-07-11 2019-11-29 郑州史戴缔机电设备有限公司 A kind of electromechanical automatic leveling system and leveling method
CN111897253A (en) * 2020-06-30 2020-11-06 北京卫星制造厂有限公司 Remote monitorable multi-axis cooperative intelligent controller based on 5G technology
CN113170972A (en) * 2021-03-26 2021-07-27 浙江乐歌智能驱动科技有限公司 Multi-upright-column lifting system based on bus structure and identification control method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107246848A (en) * 2017-04-21 2017-10-13 江西省高速公路投资集团有限责任公司 A kind of constructing tunnel fracture morphology rapid detection system and its detection method
CN107352250A (en) * 2017-07-05 2017-11-17 宁夏天地奔牛实业集团有限公司 Self-leveling type belt self-movable foot end and belt self-movable foot end self-leveling method
CN108829041A (en) * 2018-07-13 2018-11-16 安徽工程大学 A kind of numerically-controlled machine tool multi-axis controller of self-stabilization
CN110515397A (en) * 2019-07-11 2019-11-29 郑州史戴缔机电设备有限公司 A kind of electromechanical automatic leveling system and leveling method
CN111897253A (en) * 2020-06-30 2020-11-06 北京卫星制造厂有限公司 Remote monitorable multi-axis cooperative intelligent controller based on 5G technology
CN111897253B (en) * 2020-06-30 2022-01-04 北京卫星制造厂有限公司 Remote monitorable multi-axis cooperative intelligent controller based on 5G technology
CN113170972A (en) * 2021-03-26 2021-07-27 浙江乐歌智能驱动科技有限公司 Multi-upright-column lifting system based on bus structure and identification control method

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CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20160413

Termination date: 20161023