Anti-collision fender function controller
By designing anti-collision pad function controllers and using components such as PLC controllers and air compressors, the difficulties in the anti-collision pad system in inspection and control are solved, and efficient operation processes and emergency support are achieved.
Patent Information
- Application Number
- CN202411811590.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-10
- Publication Date
- 2025-04-15
AI Technical Summary
The existing anti-collision pad system has difficulties in inspection and control, including troublesome pipeline connections, high labor consumption, inconvenient fault handling, and the lack of effective solutions when the intelligent water and gas control device fails.
A functional controller for anti-collision pads is designed, using PLC controller, air compressor, cable and sensors. Through simplified cable connection, the control and inspection of valves in the anti-collision pads are realized, providing emergency support, and reducing manpower consumption and improving operating efficiency through an automated system.
It realizes simple inspection and control of anti-collision pads, improves operating efficiency, reduces manpower consumption, and provides independent control emergency guarantee when the intelligent water and gas control device fails.
Smart Images
Figure CN119828529A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of anti-collision bumper pad function controllers, in particular to an anti-collision bumper pad function controller. Background Art
[0002] The auxiliary facilities for large ship T-shaped docking are equipped with two sets of intelligent water and gas control devices, six sets of actuators, and three anti-collision pads. The three are connected through pipelines to realize the injection and drainage of the anti-collision pads and the injection and exhaust of the anti-collision pads, and realize the draft and internal pressure adjustment of the anti-collision pads. The intelligent water and gas control devices and actuators are fixedly installed, and the anti-collision pads are movable equipment. The anti-collision pads are placed on special storage racks when not in operation, and are hung around the actuators when in operation, so as to facilitate the actuators to inject water and gas and electrical control of the anti-collision pads.
[0003] Because the anti-collision pad is large in size and far away from the actuator, it is troublesome to connect the pipelines between the two when inspecting the anti-collision pad, which makes inspection difficult; and because the drain valve, exhaust valve, internal pressure sensor, draft sensor and other components inside the anti-collision pad must be powered on for testing, the actual inspection of the anti-collision pad consumes manpower and material resources, which is not conducive to improving on-site operation efficiency. When the equipment is performing ship T docking operations, if there is a serious failure of the intelligent water and gas device, the anti-collision pad has no other control method, which may have harmful effects. Traditionally, the control cable is directly connected to the actuator and the anti-collision pad at the output end of the actuator, which consumes a lot of manpower and material resources, and the existing solution will cause more serious wear on the cable, which is not conducive to maintaining the reliability of the equipment. In addition, when the intelligent water and gas control device for ship T docking operations fails, there is no effective solution. Summary of the invention
[0004] 1. Technical issues to be resolved In view of the deficiencies of the prior art, the present invention provides an anti-collision bumper function controller to solve the problems raised in the above background technology.
[0005] (II) Technical solution To achieve the above-mentioned objectives, the present invention provides the following technical solutions: a collision avoidance pad function controller, comprising a PLC controller, an air compressor, and a cable, wherein a side cover, an HMI touch screen, an operating knob, a temperature and humidity sensor, a light intensity sensor, and an aviation socket are fixedly installed on the PLC controller, a terminal post is fixedly installed on the inner side of the side cover, a compressed air source pipeline is fixedly connected to the exhaust port of the air compressor, one end of the cable is electrically connected to the aviation socket, the compressed air source pipeline is connected to the collision avoidance pad inflation pipeline on the collision avoidance pad through an air injection pipeline, a pad terminal box is fixedly installed on the collision avoidance pad, the pad terminal box is electrically connected to the other end of the cable, and the PLC controller and the air compressor are electrically connected through the electronic connecting wire in the junction box.
[0006] Preferably, the sensor is a temperature and humidity sensor or a light intensity sensor.
[0007] Preferably, the PLC controller is electrically connected to the HMI touch screen, operating knob, sensor, and aviation socket.
[0008] Preferably, aviation plugs are fixedly installed at both ends of the cable, and an aviation socket is fixedly installed on the pad terminal box. The aviation plugs at both ends of the cable are plug-in electrically connected to the pad terminal box and the aviation socket on the PLC controller.
[0009] Preferably, the gas injection pipeline adopts a PU hose.
[0010] Preferably, the cable is a highly flexible drag chain cable.
[0011] Preferably, a valve is fixedly installed on the compressed air source pipeline.
[0012] Preferably, the terminal posts in the side cover are electrically connected to the HMI touch screen, the operating knob, the sensor, the aviation plug socket and the junction box.
[0013] Compared with the prior art, the present invention provides an anti-collision pad function controller, which has the following beneficial effects: 1. The anti-collision pad function controller can realize the switch action of the drainage valve and the exhaust valve in the anti-collision pad, and check the internal pressure sensor and the draft depth sensor through a simple cable connection; 2. The anti-collision pad function controller increases emergency protection (reliability). When it fails, the anti-collision pad function controller can be used to achieve independent control of the anti-collision pad. When the aviation plug connection fails, the terminal can be used to control the valve separately; 3. The anti-collision pad function controller does not need to connect the anti-collision pad with the actuator through the original heavy pipeline, which reduces manpower consumption. The system automatically performs the three-seat fender inflation and pressure maintenance test, and the automatic internal pressure adjustment and automatic inspection can save manpower consumption and time; 4. The anti-collision fender function controller automatically performs inflation and pressure-maintaining tests on the three-seat fenders through the system. Automatic internal pressure adjustment and automatic inspection can be performed by non-specific trained personnel. BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Figure 1 It is a structural schematic diagram of the present invention.
[0015] In the figure: 1. Anti-collision pad function controller; 2. Side cover; 3. HMI touch screen; 4. Operation knob; 5. Sensor; 6. Aviation plug socket; 7. Valve; 8. Air compressor; 9. Compressed air source pipeline; 10. Cable; 11. Junction box; 12. Air injection pipeline; 13. Anti-collision pad inflation pipeline; 14. Pad terminal box. DETAILED DESCRIPTION
[0016] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0017] like Figure 1 As shown, the present invention provides a technical solution: an anti-collision bumper function controller, comprising a PLC controller 1, a side cover 2, an HMI touch screen 3, an operating knob 4, a sensor 5, an aviation plug socket 6, a valve 7, an air compressor 8, a compressed air source pipeline 9, a cable 10, a junction box 11, an air injection pipeline 12, an anti-collision bumper inflation pipeline 13, and a bumper terminal box 14. The PLC controller 1 is fixedly mounted with a side cover 2, an HMI touch screen 3, an operating knob 4, a temperature and humidity sensor, a light intensity sensor 5, an aviation plug socket 6, a valve 7, an air compressor 8, a compressed air source pipeline 9, a cable 10, a junction box 11, an air injection pipeline 12, an anti-collision bumper inflation pipeline 13, and a bumper terminal box 14. Plug socket 6, the inner side of the side cover 2 is fixedly installed with a terminal post, the exhaust port of the air compressor 8 is fixedly connected to the compressed air source pipeline 9, one end of the cable 10 is electrically connected to the aviation socket 6, the compressed air source pipeline 9 is connected to the anti-collision pad inflation pipeline 13 on the anti-collision pad through the air injection pipeline 12, a bumper pad terminal box 14 is fixedly installed on the anti-collision pad, the bumper pad terminal box 14 is electrically connected to the other end of the cable 10, and the PLC controller 1 and the air compressor 8 are electrically connected through the electronic connecting line in the junction box 11.
[0018] Furthermore, the sensor 5 is a temperature and humidity sensor and a light intensity sensor.
[0019] Through the above technical solution, the temperature and humidity sensor adopts the THE110 model, and the light intensity sensor adopts the TEMT6000 model, and the environmental data is detected through the temperature and humidity sensor and the light intensity sensor.
[0020] Furthermore, the PLC controller 1 is electrically connected to the HMI touch screen 3 , the operation knob 4 , the sensor 5 , and the aviation socket 6 .
[0021] Through the above technical solution, the drain valve, exhaust valve, internal pressure sensor and draft sensor are fixedly installed on the anti-collision pad. The drain valve and exhaust valve are solenoid valves. The drain valve, exhaust valve, internal pressure sensor and draft sensor fixedly installed on the anti-collision pad are tested and data is transmitted through the HMI touch screen 3 and the operation knob 4.
[0022] Furthermore, aviation plugs are fixedly installed at both ends of the cable 10, and an aviation socket 6 is fixedly installed on the bumper terminal box 14. The aviation plugs at both ends of the cable 10 are plug-in electrically connected to the bumper terminal box 14 and the aviation socket 6 on the PLC controller 1.
[0023] Through the above technical solution, the anti-collision pad and the PLC controller 1 are electrically connected through the cable 10 to transmit data.
[0024] Furthermore, the gas injection pipeline 12 adopts a PU hose.
[0025] Furthermore, the cable 10 adopts a highly flexible drag chain cable.
[0026] Furthermore, a valve 7 is fixedly installed on the compressed air source pipeline 9 .
[0027] Through the above technical solution, the valve 7 is a gas injection solenoid valve, which is electrically connected to the junction box 11 , and the opening and closing of the valve 7 is controlled by the PLC controller 1 .
[0028] Furthermore, the terminal in the side cover 2 is electrically connected to the HMI touch screen 3 , the operation knob 4 , the sensor 5 , the aviation socket 6 and the junction box 11 .
[0029] Through the above technical solution, when the whole fails, the terminal inside the side cover 2 can be used for emergency connection.
[0030] Working principle: First, when the inflation pressure test starts, the PLC controller 1 reads the 4-20mA signal of the internal pressure sensor of the three fenders respectively, converts it into the current ball internal pressure and displays it on the HMI touch screen 3, and at the same time determines whether the current pressure reaches the pressure test pressure. If the current internal pressure of a fender is greater than the pressure holding pressure, the anti-collision fender exhaust valve is opened to exhaust. If the current internal pressure is less than the pressure holding pressure, the gas injection solenoid valve is opened to inject gas. The internal air pressure of each fender is adjusted to the pressure holding pressure one by one and then left to stand for 1 hour. After internal rebalancing, the internal pressure is adjusted to the test pressure by exhaust or gas injection, and the timing is started and the internal pressure change is recorded. After the timing ends, it is determined whether the pressure test is passed by the internal pressure change, and the result is displayed on the HMI touch screen 3; when the automatic When adjusting the internal pressure, the PLC controller 1 reads the reading of the internal pressure sensor of the anti-collision pad, converts it to obtain the current ball internal pressure value, and then adjusts the internal pressure to the set value through the aforementioned injection and exhaust process, and displays the result on the HMI touch screen 3; when starting automatic inspection, the PLC controller 1 reads the reading of the internal pressure sensor of the anti-collision pad, converts it to obtain the current ball internal pressure value, and approaches the stored air pressure value according to the internal pressure value. By collecting data from the temperature and humidity sensor and the light intensity sensor as a reference, the reasonable range of internal pressure change when inflation and deflation are performed for a certain period of time is calculated and compared with the actual result. If the actual result exceeds the reasonable range of the calculation, it is reviewed according to the set number of repetitions. If the review result still does not meet the standard, the staff is reminded.
[0031] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A collision prevention pad function controller, comprising a PLC controller (1), an air compressor (8), and a cable (10), characterized in that: The PLC controller (1) is fixedly mounted with a side cover (2), an HMI touch screen (3), an operating knob (4), a temperature and humidity sensor, a light intensity sensor (5), and an aviation socket (6); a terminal post is fixedly mounted on the inner side of the side cover (2); an exhaust port of the air compressor (8) is fixedly connected to a compressed air source pipeline (9); one end of the cable (10) is electrically connected to the aviation socket (6); the compressed air source pipeline (9) is connected to an anti-collision pad inflation pipeline (13) on the anti-collision pad via an air injection pipeline (12); a pad terminal box (14) is fixedly mounted on the anti-collision pad; the pad terminal box (14) is electrically connected to the other end of the cable (10); and the PLC controller (1) and the air compressor (8) are electrically connected via an electronic connection line in the terminal box (11).
2. The anti-collision pad function controller according to claim 1, characterized in that: The sensors (5) are temperature and humidity sensors and light intensity sensors.
3. The anti-collision pad function controller according to claim 1, characterized in that: The PLC controller (1) is electrically connected to the HMI touch screen (3), the operating knob (4), the sensor (5), and the aviation plug socket (6).
4. The anti-collision pad function controller according to claim 1, characterized in that: Aviation plugs are fixedly mounted on both ends of the cable (10), an aviation socket (6) is fixedly mounted on the bumper terminal box (14), and the aviation plugs at both ends of the cable (10) are pluggably electrically connected to the bumper terminal box (14) and the aviation socket (6) on the PLC controller (1).
5. The anti-collision pad function controller according to claim 1, characterized in that: The gas injection pipeline (12) adopts a PU hose.
6. The anti-collision pad function controller according to claim 1, characterized in that: The cable (10) is a highly flexible drag chain cable.
7. The anti-collision pad function controller according to claim 1, characterized in that: A valve (7) is fixedly installed on the compressed air source pipeline (9).
8. The anti-collision pad function controller according to claim 1, characterized in that: The terminal posts in the side cover (2) are electrically connected to the HMI touch screen (3), the operating knob (4), the sensor (5), the aviation plug socket (6) and the junction box (11).