A digital simulation installation method for a hatch cover

By combining a total station with precision analysis and control software, digital simulation installation of the hatch cover system was achieved, solving the problem of manual measurement errors and improving the installation accuracy and construction efficiency of the hatch cover.

CN118723007BActive Publication Date: 2025-11-07GUANGZHOU WENCHONG SHIPYARD CO LTD
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Patent Information

Application Number
CN202410958382.2
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-07-17
Publication Date
2025-11-07
Estimated Expiration
2044-07-17

AI Technical Summary

Technical Problem

In existing technologies, there are errors in the data measured manually for hatch cover systems and in simulated installation, which affects construction efficiency and quality.

Method used

The installation data of the hatch cover and hatch coaming were collected using a total station. Accuracy analysis and control software was used to analyze the assembly and splicing, adjust the hatch cover compression amount, and export relevant drawings for on-site construction.

Benefits of technology

It reduces the accuracy error caused by manual measurement, improves the installation accuracy and construction efficiency of hatch covers, improves the construction environment, and reduces the risk factor and cross-operations.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to the technical field of shipbuilding, and discloses a hatch digital simulation installation method, comprising the following steps: S1, after the hatch is completed, using a total station to collect installation data of each outfitting part; S2, using the total station to collect position data of each outfitting part; S3, measuring closing data of the hatch; S4, using precision analysis control software to close and splice data of the installation data and the ship coordinate system, checking the precision of the theoretical data of the closing measurement point in the splicing data and the closing data in step S3; S5, using the precision analysis control software to close and analyze the position data and the splicing data in step S4, and matching and adjusting the hatch compression amount; S6, adjusting the coordinate system of the installation of each outfitting part, adjusting from the ship coordinate system to the cargo hold coordinate system, and exporting an outfitting part installation measurement table; and S7, performing installation operation on the construction site. The precision error caused by manual measurement is reduced, and the hatch installation precision and construction efficiency are improved.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of shipbuilding, in particular to a hatch cover digital simulation installation method. BACKGROUND

[0002] In the process of shipbuilding, the hatch cover of a cargo ship is a closing device of the opening of the deck of the ship, and plays a role of sealing the hatch, protecting the cargo and partially supporting the platform. The strength and sealing performance of the hatch cover affect the safety of the ship and the time of loading and unloading the cargo, and are related to the economy of the ship.

[0003] The hatch cover system of the ship mainly includes a hatch coaming and a hatch cover during construction, and the installation accuracy of the two affects the quality of the construction of the hatch cover system. In the prior art, the data of the hatch cover and the hatch coaming are obtained by manual measurement during construction, and the installation of the hatch cover is simulated manually. However, manual measurement has errors and is not reproducible, which leads to unqualified installation accuracy of the outfitting parts during assembly, and may result in rework, thereby affecting the construction efficiency and quality of the hatch cover system. SUMMARY

[0004] The purpose of the present application is to provide a hatch cover digital simulation installation method to solve the problem of errors in manual measurement of the data of the hatch cover system and simulation installation in the prior art, which affects the construction efficiency and quality.

[0005] In order to achieve the above-mentioned purpose, the present application provides a hatch cover digital simulation installation method, comprising the following steps:

[0006] S1, after the hatch cover is finished, determining the measurement control points of each outfitting part based on the hatch cover, and collecting the installation data of each outfitting part by using a total station;

[0007] S2, after the cargo hold of the ship is formed, determining the installation position points of each outfitting part on the hatch coaming according to the theoretical installation position of the outfitting part, the installation position points corresponding to the measurement control points, and collecting the position data of each outfitting part by using a total station;

[0008] S3, determining the closing measurement points of the hatch cover, and measuring the closing data of the closing measurement points;

[0009] S4, applying precision analysis control software to splice the installation data of the measurement control points in step S1 and the ship coordinate system, and checking the precision of the theoretical data of the closing measurement points in the spliced data and the closing data of the closing measurement points in step S3 by using the precision analysis control software;

[0010] S5, applying the precision analysis control software to splice the position data of the installation position points in step S2 and the spliced data in step S4, and matching and adjusting the compression amount of the hatch cover;

[0011] S6, adjusting the coordinate system of the installation of each fitting on the hatch cover, adjusting from the hull coordinate system to the cargo hold coordinate system, and deriving a fitting installation measurement table and an accessory adjusting pad measurement table;

[0012] S7, performing on-site installation work at the construction site according to the fitting installation measurement table and the accessory adjusting pad measurement table in step S6.

[0013] Preferably, in step S1, the fittings include hatch cover positioning pins, guide devices or binding bridges, hatch cover transverse limiting devices, hatch cover stop devices, support block adjusting pads, compression flat irons, and separation joint compression plates, the measurement control points of the hatch cover positioning pins include at least four points on the edge of the pin hole, and the center of the pin hole is determined by the four points; the installation data of the guide devices or binding bridges include the coordinates of the adjusting pad installation surface of the measured guide devices or binding bridges; the installation data of the hatch cover transverse limiting devices include the installation position of the bevel adjusting pad of the measurer, four points are selected on each surface of the bevel adjusting pad, and the height and position of each point are measured; the measurement control points of the hatch cover stop devices include the upper surface measurement points of the stop ear plate and the intersection point of the center line of the stop ear plate and the horizontal line of the rubber groove, and the installation data of the hatch cover stop devices include the height value of the upper surface of the stop ear plate, the height value of the rubber groove of the hatch cover stop device, and the installation center point of the stop ear plate; the installation data of the support block adjusting pad include the flatness of the four corners of the support block installation seat plate, the rubber groove value, and the center value of the support block installation seat plate; the installation data of the compression flat iron include the corresponding position, the flatness of the hatch cover rubber groove, and the flatness of the corresponding position of the hatch coaming; and the installation data of the separation joint compression plate include three-dimensional coordinates, center line position, and angle value.

[0014] Preferably, the installation data measurement of the guide position or binding bridge is performed after the welding of the hatch cover is completed, and the installation data measurement of the hatch cover transverse limiting device is performed after the installation of the hatch cover transverse limiting device.

[0015] Preferably, the installation data measurement of the separation joint compression plate is performed after the folding of the hatch cover.

[0016] Preferably, in step S2, the installation positions of each fitting are drawn on the hatch coaming, installation position points are selected on the installation positions, and the flatness of the installation positions of each fitting around the hatch coaming is measured.

[0017] Preferably, in step S4, when the precision analysis control software checks the precision of the splicing data, the folding precision is ensured to be within 2 mm, and when the folding data of the folding measurement point of the hatch cover exceeds the range, the folding data of the folding measurement point is manually adjusted.

[0018] Preferably, in step S5, when matching and adjusting the compression amount of the hatch cover, three points are selected to determine the plane for the hatch cover rubber groove plane data and the hatch coaming plane data, and the adjusted plane meets the assembly precision requirements.

[0019] Preferably, in step S5, when the matching adjustment hatch compression amount does not meet the requirements, the hatch is individually adjusted by data disassembly, the hatch is made into an inclined surface, the inclination of the hatch is controlled to be less than 3 degrees, and the adjustment ensures that the hatch meets the required tolerance range.

[0020] Preferably, in step S7, the field installation operation includes: installing the hatch accessories according to the accessory installation measurement table, installing and welding the hatch and the hatch coaming accessories according to the accessory installation measurement table, post-welding inspection work, hatch coaming and hatch finishing painting operation, hatch on board, hatch accessory installation precision inspection and processing, hatch utility and hatch tightness finishing inspection.

[0021] Compared with the prior art, the hatch digital simulation installation method has the beneficial effects that: after the hatch is finished, the installation data and position data of the fittings are obtained by using a total station according to the measurement control points of the fittings on the hatch and the installation position points of the fittings on the hatch coaming, the closing and splicing analysis of the installation data, position data and closing data of the hatch are performed by using precision analysis control software, the hatch installation is simulated, the closing data precision and compression amount of the hatch meet the drawing requirements, the related drawings are exported for field construction, the precision error caused by manual measurement is reduced, the installation precision and construction efficiency of the hatch are improved, the construction environment of the hatch is improved, the danger coefficient and cross operation are reduced. BRIEF DESCRIPTION OF DRAWINGS

[0022] Figure 1 is a flowchart of the hatch digital simulation installation method of the present application;

[0023] Figure 2 is an installation data collection schematic diagram of the guide device or binding bridge of the hatch digital simulation installation method of the present application;

[0024] Figure 3 is an installation data collection schematic diagram of the hatch transverse limiting device of the present application;

[0025] Figure 4 is Figure 3 a side view of the installation data collection schematic diagram of the hatch transverse limiting device of the present application;

[0026] Figure 5 is an installation data collection schematic diagram of the hatch stop device of the present application;

[0027] Figure 6 is Figure 5 a side view of the installation data collection schematic diagram of the hatch stop device of the present application;

[0028] Figure 7is the installation data collection schematic diagram of the pressing flat iron of the hatch cover digital simulation installation method of the application;

[0029] Figure 8 is the installation data collection schematic diagram of the support block adjusting pad of the hatch cover digital simulation installation method of the application;

[0030] Figure 9 is the closing data collection schematic diagram of the closing measurement point of the hatch cover of the hatch cover digital simulation installation method of the application. DETAILED DESCRIPTION

[0031] The specific embodiments of the application are described in further detail below in combination with the drawings and examples. The following examples are used to illustrate the application, but are not used to limit the scope of the application.

[0032] A preferred embodiment of the hatch cover digital simulation installation method of the application is shown in Figures 1 to 9 The hatch cover digital simulation installation method comprises the following steps:

[0033] S1, after the completion of hatch cover manufacturing, the measurement control points of each outfitting part are determined based on the hatch cover, and the installation data of each outfitting part is collected by using a total station.

[0034] After the completion of hatch cover manufacturing, the outfitting parts on the hatch cover need to be assembled with the hatch cover as accessories. According to the number of outfitting parts and the precision control point of installation, the measurement technical requirements of each outfitting part can be formulated. The installation data of each outfitting part is collected by using a total station, which is the position of each outfitting part on the hatch cover, i.e. the assembly data relative to the hatch cover. After being collected by the total station, the data can be easily archived in electronic form.

[0035] After the completion of hatch cover manufacturing, each line on the hatch cover already exists, and the coordinate size between the measurement control points of each outfitting part on the hatch cover and the lines on the hatch cover can be measured to obtain the relevant installation data.

[0036] S2, after the formation of the ship cargo hold, the installation position points of each outfitting part are determined on the hatch coaming according to the theoretical installation position of the outfitting part, the installation position points correspond to the measurement control points, and the position data of each outfitting part is collected by using a total station.

[0037] Part of the outfitting on the hatch cover is to be assembled on the hatch coaming, the installation position points of the outfitting on the hatch coaming are determined, the position data of the outfitting is collected by the total station, the assembly position of each outfitting on the hatch coaming can be determined, and the position data is specifically the coordinate size of the installation position points relative to the hatch coaming. The installation position points correspond to the measurement control points, which can ensure the position assembly accuracy of the same outfitting on the hatch cover. In the embodiment, when the position data on the hatch coaming is measured, the flatness of the hatch coaming is measured, and the measurement points of the data of the hatch coaming need to be increased due to the small number of longitudinal hatch coaming outfitting.

[0038] S3, determining the closing measurement points of the hatch cover, and measuring the closing data of the closing measurement points.

[0039] As shown in Figure 9 , the hatch cover is usually two, and the two hatch covers form the entire hatch cover after closing. The closing measurement points are selected on the hatch cover to obtain the closing data, which can be used for modification in the digital simulation process to ensure the accuracy of the hatch cover after installation. In the embodiment, the closing data can be measured synchronously when the installation data on the hatch cover is measured in step S1 to improve the efficiency. In the embodiment, ten closing points on the hatch cover are selected, and the actual closing data of the hatch cover is recorded after measurement.

[0040] S4, applying the precision analysis control software to splice the installation data of the measurement control points in step S1 and the ship coordinate system, checking the precision of the closing measurement points in the splicing data and the closing data of the closing measurement points in step S3 by the precision analysis control software.

[0041] The precision analysis control software is used to splice the installation data and the ship coordinate system, and the precision between the installation data and the theoretical data of the closing points of the hatch cover in the ship coordinate system can be obtained by the precision analysis control software, so as to judge the closing precision and preliminarily ensure the installation accuracy of the outfitting on the hatch cover. In the embodiment, the precision analysis control software is specifically DACS software.

[0042] S5, applying the precision analysis control software to splice the position data of the installation position points in step S2 and the splicing data in step S4, and matching and adjusting the compression amount of the hatch cover.

[0043] The installation data of the hatch cover and the closing data of the hatch cover form the splicing data, and the position data on the hatch coaming obtained in step S2 is spliced and analyzed by the precision analysis control software on the basis of the data, so as to match and adjust the compression amount of the hatch cover, that is, the matching relationship between the hatch cover and the installation position on the hatch coaming after closing, and the precision of the hatch cover and the hatch coaming after adjustment meets the drawing and process requirements.

[0044] S6, adjust the coordinate system of each fitting on the hatch cover, from the hull coordinate system to the cargo hold coordinate system, and derive the fitting installation measurement table and the accessory adjustment pad measurement table.

[0045] In the application of the precision analysis control software in step S4, the fittings are data-fitted based on the hull coordinate system, while in the field construction, the coordinate system of the fittings and other accessories is based on the cargo hold, so the fitting installation measurement table and the accessory adjustment pad measurement table are derived from the hull coordinate system to the cargo hold coordinate system, which is convenient for subsequent field construction.

[0046] S7, according to the fitting installation measurement table and the accessory adjustment pad measurement table in step S6, carry out field installation work on the construction site.

[0047] Under the guidance of the fitting installation measurement table and the accessory adjustment pad measurement table, the field construction can quickly install each accessory and subsequent precision inspection and processing, etc., which improves the efficiency of field work.

[0048] The digital simulation installation method of the hatch cover, after the completion of the hatch cover, obtains the installation data and position data of the fittings according to the measurement control points of each fitting on the hatch cover and the installation position points of the fittings on the hatch coaming, carries out fitting analysis on the installation data, position data and fitting data of the hatch cover through the precision analysis control software, simulates the installation of the hatch cover, so that the fitting data precision, compression amount and other data of the hatch cover meet the requirements of the drawings, and then the related drawings are derived for field construction, which reduces the precision error caused by manual measurement, improves the installation precision and construction efficiency of the hatch cover, improves the construction environment of the hatch cover, reduces the risk coefficient and cross operation.

[0049] Preferably, in step S1, the outfitting parts include hatch cover positioning pins, guide devices or binding bridges, hatch cover transverse limiting devices, hatch cover stop devices, support block adjusting pads, pressing flat irons, separation joint pressing plates, the measurement control points of the hatch cover positioning pins include at least four points on the edges of the pin holes, and the center of the pin hole is determined by the four points; the installation data of the guide devices or the binding bridges include the coordinates of the installation surface of the adjusting pads of the guide devices or the binding bridges; the installation data of the hatch cover transverse limiting devices include the installation position of the adjusting pads of the bevels, four points are selected on each surface of the adjusting pads of the bevels, and the height and position of each point are measured; the measurement control points of the hatch cover stop devices include the measurement points on the upper surface of the stop ear plates and the intersection points of the center lines of the stop ear plates and the horizontal lines of the rubber grooves, and the installation data of the hatch cover stop devices include the height value of the upper surface of the stop ear plates, the height value of the rubber groove of the hatch cover stop device, and the installation center point of the stop ear plates; the installation data of the support block adjusting pads include the flatness of the four corners of the support block installation seat plates, the rubber groove values, and the center values of the support block installation seat plates; the installation data of the pressing flat irons include the corresponding positions, the flatness of the hatch cover rubber groove, and the flatness of the corresponding positions of the hatch coaming; and the installation data of the separation joint pressing plates include three-dimensional coordinates, center line positions, and angle values.

[0050] The installation data of different outfitting parts on the hatch cover are different when the outfitting parts are installed, and different measurement control points can be selected to collect relevant installation data according to the corresponding installation data requirements.

[0051] Specifically, when the hatch cover positioning pins are installed, the installation data requirements are Fx and Fy, at least four points on the edges of the pin holes on the hatch cover are measured, the center of the pin hole can be found by the principle of the perpendicular line of the four points, and the installation data of the hatch cover positioning pins can be obtained according to the coordinates of the center. When measuring, the four points on the pin hole are as close to the diameter as possible to form two points, and the four points are evenly distributed on the circumference of the pin hole to reduce the measurement error.

[0052] As shown in FIG. 1, Figure 2 When the guide devices or the binding bridges are installed, the installation data requirements are Fx and Fy, the coordinates of the installation surface of the adjusting pads of the binding bridges or the guide devices are measured, the installation position of the adjusting pads can be obtained, and the installation position of the guide devices or the binding bridges can be determined. Since the hatch cover has been made, the reference points on the hatch cover already exist, the values of the same positions above the adjusting pads of the binding bridges or the guide devices are simulated after being subtracted by a tolerance of 13 mm, and the thickness of the adjusting pads that need to be installed is obtained, and the height measurement of the installation position of the adjusting pads is required.

[0053] As shown in FIG. 1, Figure 3 and Figure 4As shown, the installation data of the hatch cover transverse limiting device requires Fx and Fy, and the installation position data of the accessory bevel adjusting pad needs to be measured. Four points are selected on each surface of the bevel adjusting pad, and the height and position of each point are measured to ensure that the height and position are basically consistent. Since the hatch cover accessory and the hatch cover body are both in the form of a bevel groove, the height direction is based on the edge of the bevel groove of the accessory, which can improve the accuracy. In this embodiment, attention should be paid to the reverse structure of the accessory and the cargo hold forming size during installation of the hatch cover transverse limiting device. When there is a large deviation in the cargo hold forming, the installation size error of the positioning pin needs to be adjusted, which is achieved by adjusting the thickness of the upper plate.

[0054] As shown, Figure 5 With Figure 6 As shown, the installation of the hatch cover stop device requires Fx, Fy and Fz data. The height value of the upper surface of the stop ear plate, the height value of the rubber groove of the hatch cover stop device, and the installation center point of the stop ear plate can be obtained by collecting the position of the intersection point of the upper surface measurement point of the stop ear plate and the center line of the rubber groove. In this embodiment, the upper surface measurement point of the center line of the stop ear plate and the center line point need to be used multiple times, and attention should be paid to the integrity of the measurement to prevent omission. The reflector needs to be placed in the appropriate position during measurement.

[0055] As shown, Figure 8 The installation of the support block adjusting pad requires Fx, Fy and Fz, and the installation data of the support block adjusting pad can be obtained by collecting the Fx, Fy and Fz values of the four corner flatness, rubber groove value and center value of the support block mounting seat plate. In this embodiment, the measurement points need to be complete, and the positions measured correspond one by one to the point positions measured by the hatch coaming.

[0056] As shown, Figure 7 The installation of the pressing flat iron requires Fx, Fy and Fz, i.e. its three-dimensional coordinates. The pressing flat iron is used to press various accessories, and the corresponding position is the installation position of each accessory. The installation coordinates of the pressing flat iron can be obtained by collecting the coordinates of the corresponding position. The installation height of the pressing flat iron is determined by digital simulation. In this embodiment, the number of measurement points of the pressing flat iron in the longitudinal direction of the ship should be sufficient to improve the accuracy and data integrity of the simulation installation.

[0057] The installation data of the separation wind pressing plate needs to be measured after the hatch cover is formed. The sample plate is made and installed according to the measured model.

[0058] Preferably, the installation data measurement of the guide position or the binding bridge is performed after the hatch cover is welded, and the installation data measurement of the hatch cover transverse limiting device is performed after the hatch cover transverse limiting device is installed.

[0059] The installation data measurement of the guide position or the binding bridge is measured after the welding of the hatch cover is completed, and the installation data measurement of the hatch cover transverse limiting device is measured after the installation of the hatch cover transverse limiting device, so that the measurement precision caused by welding deformation can be avoided.

[0060] Preferably, the installation data measurement of the separation joint pressing plate is measured after the hatch cover is closed.

[0061] The installation data of the separation joint pressing plate is measured after the hatch cover is closed, so that the error caused by the adjustment of the closed hatch cover can be reduced, and the precision of the data can be improved.

[0062] Preferably, in step S2, the installation positions of various fittings are drawn on the hatch coaming, the installation position points are selected on the installation positions, and the flatness of the installation positions of various fittings around the hatch coaming is measured.

[0063] The flatness of the installation positions of various fittings around the hatch coaming is measured, so that the angle during the installation of the fittings can be simulated, and the digital simulation installation precision of the fittings can be improved. Since there are fewer longitudinal hatch coaming fittings, the number of installation position points of the hatch coaming is increased, and the installation position points and the measurement control points of various fittings of the hatch cover are corresponded as much as possible in the transverse and longitudinal directions.

[0064] Preferably, in step S4, when the precision analysis control software checks the precision of the spliced data, the closing precision is ensured to be within 2 mm, and when the closing data of the closing measurement points of the hatch cover exceeds the range, the closing data of the closing measurement points is manually adjusted.

[0065] When the closing precision exceeds 2 mm, the closing data of the hatch cover during the closing is manually adjusted in the precision analysis control software, so that the closing data matches the theoretical data, and the closing data precision is within 2 mm, so that the installation data of various fittings on the hatch cover in step S1 can be accurately determined.

[0066] Preferably, in step S5, when the closing data of the hatch cover is matched and adjusted, three points of the hatch cover rubber groove plane data and the hatch coaming plane data are determined to determine a plane, and the adjusted plane meets the assembly precision requirement.

[0067] After the hatch cover is spliced and closed, the closing data of the hatch cover is simulated and installed with the hatch coaming, the rubber groove plane of the hatch cover is in contact with the hatch coaming plane, and the precision can be ensured to meet the drawing and process requirements by adjusting the two planes to match.

[0068] Preferably, in step S5, when the matched and adjusted closing data of the hatch cover does not meet the requirement, the data of the hatch cover is separately adjusted, the hatch cover is made into an inclined surface, the inclination of the hatch cover is controlled to be less than 3 degrees, and the adjustment ensures that the hatch cover meets the required tolerance range.

[0069] When the hatch coaming plane deviation of the whole cargo hold is large, the data of the whole hatch cover is split into single block hatch cover data for angle adjustment, and after the adjustment, all the numbers of the hatch cover can be ensured to meet the tolerance range required by the drawing, and in general, the tolerance range is ±6mm.

[0070] Preferably, in step S7, the field installation operation includes: installing the hatch cover accessories according to the accessory installation measurement table, installing and welding the hatch cover and the hatch coaming accessories according to the accessory installation measurement table, and performing post-welding inspection work, hatch coaming and hatch cover finishing painting operation, hatch cover on board, hatch cover accessory installation precision inspection and processing, and hatch cover utility and hatch cover tightness finishing inspection.

[0071] In summary, the embodiment of the present application provides a kind of digital simulation installation method of hatch cover, after the hatch cover is finished, according to the measurement control point of each accessory on the hatch cover and the installation position point of the accessory on the hatch coaming, the installation data and position data of the accessory are obtained using total station, the closing data of the hatch cover is analyzed by precision analysis control software to the installation data, position data and closing data, the installation of hatch cover is simulated, so that the closing data precision, compression amount and other data of hatch cover meet the drawing requirements, then export related drawings for field construction, reduce the precision error caused by manual measurement, improve the installation precision and construction efficiency of hatch cover, improve the construction environment of hatch cover, reduce the risk coefficient and cross operation.

[0072] The above only describes the preferred embodiments of the present application, and it should be noted that for ordinary skilled in the art, without departing from the technical principles of the present application, several improvements and replacements can be made, and these improvements and replacements should be considered as the protection scope of the present application.

Claims

1. A method of digitally simulating installation of a hatch cover, characterized by, The method comprises the following steps: S1, after the hatch cover is completed, measurement control points of each fitting are determined based on the hatch cover, and installation data of each fitting is collected by using a total station instrument; S2, after the cargo hold of the ship is shaped, installation position points of each fitting are determined on the hatch coaming according to the theoretical installation position of the fitting, the installation position points correspond to the measurement control points, and position data of each fitting is collected by using the total station instrument; S3, a closing measurement point of the hatch cover is determined, and closing data of the closing measurement point is measured; S4, the installation data of the measurement control points in step S1 and the ship coordinate system are spliced by using precision analysis control software, the precision of the closing data of the closing measurement point in step S3 and the theoretical data of the closing measurement point in the spliced data is checked by using the precision analysis control software; S5, the position data of the installation position points in step S2 and the spliced data in step S4 are closed and analyzed by using the precision analysis control software, and the compression amount of the hatch cover is matched and adjusted; S6, the coordinate system of the installation of each fitting on the hatch cover is adjusted from the ship coordinate system to the cargo hold coordinate system, and a fitting installation measurement table and an accessory adjusting pad measurement table are derived; S7, the fitting installation measurement table and the accessory adjusting pad measurement table in step S6 are used to perform on-site installation operation at a construction site.

2. The digital mockup installation method of a hatch cover according to claim 1, wherein, In step S1, the fitting includes a hatch cover positioning pin, a guide device or a binding bridge, a hatch cover transverse limiting device, a hatch cover stop device, a supporting block adjusting pad, a compression flat iron, and a separation joint compression plate, the measurement control points of the hatch cover positioning pin include at least four points on the edge of a pin hole, and the center of the pin hole is determined by the four points, the installation data of the guide device or the binding bridge includes the coordinates of the adjusting pad installation surface of the guide device or the binding bridge, the installation data of the hatch cover transverse limiting device includes the installation position of the adjusting pad of the device, four points are selected on each surface of the adjusting pad, and the height and position of each point are measured, the measurement control points of the hatch cover stop device include the upper surface measurement point of a stop ear plate and the intersection point of the center line of the stop ear plate and the horizontal line of a rubber groove, the installation data of the hatch cover stop device includes the height value of the upper surface of the stop ear plate, the height value of the rubber groove of the hatch cover stop device, and the installation center point of the stop ear plate, the installation data of the supporting block adjusting pad includes the flatness of the four corners of a supporting block installation seat plate, the rubber groove value, and the center value of the supporting block installation seat plate, the installation data of the compression flat iron includes the corresponding position, the flatness of the hatch cover rubber groove, and the flatness of the corresponding position of the hatch coaming, and the installation data of the separation joint compression plate includes three-dimensional coordinates, a center line position, and an angle value.

3. The digital mockup installation method of a hatch cover according to claim 2, wherein, The installation data of the guide device or the binding bridge is measured after the hatch cover is welded, and the installation data of the hatch cover transverse limiting device is measured after the hatch cover transverse limiting device is installed.

4. The digital mockup installation method of a hatch cover according to claim 2, wherein, The installation data of the separation joint compression plate is measured after the hatch cover is closed.

5. The digital mockup installation method of a hatch cover according to any one of claims 1 to 4, characterized in that, In step S2, the installation position of each fitting is drawn on the hatch coaming, an installation position point is selected on the installation position, and the flatness of the installation position of each fitting around the hatch coaming is measured.

6. The digital mockup installation method of a hatch cover according to any one of claims 1 to 4, characterized in that, In step S4, the precision of the spliced data is checked by the precision analysis control software, to ensure that the closing precision is within 2 mm. When the closing data of the closing measurement points of the hatch cover exceeds the range, the closing data of the closing measurement points is manually adjusted.

7. The digital mockup installation method of a hatch cover according to any one of claims 1 to 4, characterized in that, In step S5, when the matching adjustment of the hatch cover compression amount is not satisfied, the hatch cover is separately adjusted by data disassembly, the hatch cover is made into an inclined surface, the inclination of the hatch cover is controlled to be less than 3 degrees, and the adjustment ensures that the hatch cover satisfies the required tolerance range.

8. The digital mockup installation method of a hatch cover according to claim 7, wherein, In step S7, the on-site installation operation includes: installing the hatch cover accessories according to the attachment installation measurement table, installing and welding the hatch cover and the hatch coaming accessories according to the attachment installation measurement table, and performing post-welding inspection work; hatch coaming and hatch cover finishing painting operation and hatch cover on board; hatch cover accessory installation precision check and processing; hatch cover utility and hatch cover tightness completion inspection.

9. The digital mockup installation method of a hatch cover according to any one of claims 1 to 4, characterized in that, ​

Citation Information

Patent Citations

  • Container ship hatch cover positioning pin advanced installation precision control method

    CN114194355A

  • Large box cabin cover three-dimensional digital simulation matching installation precision management method

    CN118107745A