Effect of Coil Width on Deformed Shape and Processing Efficiency during Ship Hull Forming by Induction Heating

The main hull of a ship is made up of a large number of plates with complex curvatures. Line heating is one of the main approaches used in the forming of a ship hull plate. Because line heating is based on manual heating using a handheld oxyacetylene gun, the typical heating width is extremely narrow. With the development of computer control technology, a newly developed automated plate forming equipment is available and its heat source is typically an electromagnetic induction coil. The temperature field and the induction coil size are correlated. However, investigations into the induction coil size are scarce. In this study, the effect that the induction coil width has on both the forming shape and processing efficiency is investigated via simulation and test. The results show that a moderate expansion of the induction coil width at different input powers has an insignificant impact on forming shapes that is attainable by common line heating. However, as the heating width expands with the expansion of the induction coil width, the number of the processing lines via line heating is reduced which improves the processing efficiency.


Introduction
During ship manufacturing, many plates with complex curvatures must be formed for the main hull of a ship, which is a time-consuming process. During this process, the line heating method creates local contraction deformation in a plate via a localized heating source, of which width is significantly narrower in size than the plate length or width as this processing method is based on moving a handheld oxyacetylene gun over a processed plate. In addition, it is believed that a narrower flame is beneficial to the formation of plate shapes with small curvatures. This method is widely deployed.
It is difficult to control the heat input when using a flame heat source. For line heating-based automated forming equipment, an electromagnetic induction heating has become a new heat source for the hot forming of ship hull plates because it is easy to control. Ueda [1,2] investigated the pattern of ship hull plates forming by line heating, discussed the heating line deployment principle and the heating criteria based on the theory of inherent strain, and verified and modified the path produced via induction heating. This work laid the foundation for the development of automated line heating forming equipment for ship hull plates. With the successful development of an automated system for ship hull plates forming by line heating [3], induction heating devices are gradually replacing manual oxyacetylene guns and are becoming a common heat source in line heating processing. Induction The induction heating frequency used for ship hull forming is usually 8-50 kHz. When current flows through an inductor that is near a steel workpiece, an eddy current is induced at the surface of the plate. Induction heat is generated in the plate.
The eddy current during induction heating can be given by Maxwell's equations in the frequency domain as [12]: where stands for permeability, is the magnetic vector potential, is the angular velocity, is the electric conductivity and is the external current. The magnetic vector potential can be obtained from Equation (1) when the external current is given. The resistance heat generated by the eddy current in the plate can be obtained as follows: where refers to eddy current density and can be described as = (− ).
For induction heating, the eddy current generated inside the steel plate is mainly concentrated on the plate surface. For a plate during induction heating, the heat flux can be considered as a surface heat source and obtained as follows: refers to the heat flux on the surface of the steel plate and denotes the plate thickness. The heat flux calculated before is used as the initial input for thermal analysis. The heat flow in a plate can be expressed as follows: where refers to density, is the specific heat capacity, is the temperature of the plate and is the thermal conductivity. Thermal deformation calculation is followed after the temperature field, which is treated as the thermal load obtained from Equation (4).
The basic equations related to mechanical analysis are considered as follows: , + = 0 (5) where refers to stress tensor and represents the body force. The induction coil used in this study is shown in Figure 2. The entire coil is divided equally into three internal frames, as shown in Figure 2a. Considering plate bending deformation, the coil is designed to be slightly curved, and the horizontal curvature radius is 1000 mm. The coil projection The induction heating frequency used for ship hull forming is usually 8-50 kHz. When current flows through an inductor that is near a steel workpiece, an eddy current is induced at the surface of the plate. Induction heat is generated in the plate.
The eddy current during induction heating can be given by Maxwell's equations in the frequency domain as [12]: 1 where µ stands for permeability, A is the magnetic vector potential, ω is the angular velocity, σ is the electric conductivity and J S is the external current. The magnetic vector potential A can be obtained from Equation (1) when the external current J S is given. The resistance heat generated by the eddy current in the plate can be obtained as follows: where J e refers to eddy current density and can be described as J e = σ(− ∂A ∂t ). For induction heating, the eddy current generated inside the steel plate is mainly concentrated on the plate surface. For a plate during induction heating, the heat flux can be considered as a surface heat source and obtained as follows: where q refers to the heat flux on the surface of the steel plate and t denotes the plate thickness. The heat flux calculated before is used as the initial input for thermal analysis. The heat flow in a plate can be expressed as follows: where ρ refers to density, c is the specific heat capacity, T is the temperature of the plate and λ is the thermal conductivity. Thermal deformation calculation is followed after the temperature field, which is treated as the thermal load obtained from Equation (4). The basic equations related to mechanical analysis are considered as follows: where σ ij refers to stress tensor and F bi represents the body force. The stress-strain relationship can be expressed as: where {dσ} refers to the stress increment, [D] is the elastoplastic matrix, {dε} is the strain increment, {C} is the thermal stiffness matrix and dT is the temperature increment. Deformation of the plate can be obtained by solving the equations under actual boundary conditions. The induction coil used in this study is shown in Figure 2. The entire coil is divided equally into three internal frames, as shown in Figure 2a. Considering plate bending deformation, the coil is designed to be slightly curved, and the horizontal curvature radius is 1000 mm. The coil projection outer edge width is L C = 220 mm, the outer edge length is L B = 200 mm, and L B is the direction of coil movement. The dimensions of the plate are 1000 mm × 800 mm × 16 mm (L × B × t). The element type of the plate is DC3D8 for heat transfer simulation and C3D8R for deformation calculation. Fine grids are generated near the heating lines and the element size is 5 mm × 5 mm × 4 mm. Sparse grids are generated away from the heating lines and the element size is 50 mm × 20 mm × 8 mm. Transitional grids are generated between them and the whole model consists of 68,600 elements and 86,399 nodes. The rigid body displacement of the plate is constrained during the calculation.

Induction Heating Experiment
To verify the accuracy of the finite element method, an induction heating test is designed. In this test, an experimental platform made of triaxial motion of the coil is developed that can easily control the coil's positioning, motion direction and travel speed over the test plate. The positioning precision of the experimental platform is 1 mm; and the controllable speed precision is 1 mm/s. To ensure a stable distance between the coil and the plate after plate deformation, the coil is embedded in the frame of a small vehicle, and the trolley wheel of the vehicle maintains rolling contact with the plate, which ensures no contact between the coil and plate, as shown in Figure 2b. For the initial condition, the lowest position of the coil center is 5 mm from the bottom of the trolley wheel. The experimental platform and test scenario are shown in Figure 3. The dimensions of the plate are 1000 mm × 800 mm × 16 mm (L × B × t). The element type of the plate is DC3D8 for heat transfer simulation and C3D8R for deformation calculation. Fine grids are generated near the heating lines and the element size is 5 mm × 5 mm × 4 mm. Sparse grids are generated away from the heating lines and the element size is 50 mm × 20 mm × 8 mm. Transitional grids are generated between them and the whole model consists of 68,600 elements and 86,399 nodes. The rigid body displacement of the plate is constrained during the calculation.

Induction Heating Experiment
To verify the accuracy of the finite element method, an induction heating test is designed. In this test, an experimental platform made of triaxial motion of the coil is developed that can easily control the coil's positioning, motion direction and travel speed over the test plate. The positioning precision of the experimental platform is 1 mm; and the controllable speed precision is 1 mm/s. To ensure a stable distance between the coil and the plate after plate deformation, the coil is embedded in the frame of a small vehicle, and the trolley wheel of the vehicle maintains rolling contact with the plate, which ensures no contact between the coil and plate, as shown in Figure 2b. For the initial condition, the lowest position of the coil center is 5 mm from the bottom of the trolley wheel. The experimental platform and test scenario are shown in Figure 3. The test plate is carbon steel, of which major thermal, physical and mechanical properties are listed in Table 1 and Table 2 which is similar to Reference [13]. The plate dimensions are as follows: the length L = 1000 mm, the width B = 800 mm, and the thickness t = 16 mm. L is the coil movement direction over the plate. Here, LC/B = 0.275.
In the test, the heating line is the upper surface central line along the plate width direction (i.e., B/2). The coil length LB is aligned with the plate length L and is moved along the heating line. In the test, the electromagnetic induction frequency is 15 kHz, the heat source output power is 60 kW, and the coil travel speed is 5 mm/s. As the coil moves over the plate surface in a small rolling vehicle, the distance between the coil and the plate during heating is essentially constant.  The test plate is carbon steel, of which major thermal, physical and mechanical properties are listed in Tables 1 and 2 which is similar to Reference [13]. The plate dimensions are as follows: the length L = 1000 mm, the width B = 800 mm, and the thickness t = 16 mm. L is the coil movement direction over the plate. Here, L C /B = 0.275. In the test, the heating line is the upper surface central line along the plate width direction (i.e., B/2). The coil length L B is aligned with the plate length L and is moved along the heating line. In the test, the electromagnetic induction frequency is 15 kHz, the heat source output power is 60 kW, and the coil travel speed is 5 mm/s. As the coil moves over the plate surface in a small rolling vehicle, the distance between the coil and the plate during heating is essentially constant.
In the test, the infrared temperature sensor (with a measurement range of 250-1450 • C) detects the plate temperature change during heating, as shown in Figure 3. Temperature sensors are deployed on one side and at the rear of the coil, and they move together with the coil, i.e., temperature sensors C 1 and C 2 in Figure 3. The point measured by C 2 is 20 mm from the coil rear edge. A fixed temperature measurement point is deployed on one side of the plate to measure the temperature variation at the plate center T 1 . The final deformation of the plate is measured via a three-dimensional laser scanner measurement system after the entire plate cools to room temperature.
At the initial stage of the test, the entire coil is placed over the plate, and the trailing edge of the movement direction coincides with the plate's rear end. As the coil moves continuously, the first notable phenomenon is the upward bending deformation of the plate along the B direction. In contrast, the plate deformation along the L direction is smaller and demonstrates a downward-bending trend. This phenomenon continues until the coil has completed its movement over the entire heating line. After the entire coil moves away from the plate and the plate temperature drops, the upward-bending deformation of the plate along the B direction changes slightly. However, the downward bending of the plate along the L direction gradually becomes prominent, and the plate eventually becomes saddle-shaped. In the study, similar tests are performed under other conditions with different plate thicknesses, heat source input powers and the coil movement speeds, with essentially the same results.
Although both the side ratio and shape of the coil and plate are close, the constraints from plate regions outside the heat expansion area on the coil-induced heat expansion of the plate are different along the L and B directions because the coil motion is directional; i.e., the coil moves along the plate's L direction, as shown in Figure 4. Under the local contraction force P B along the B direction, the plate bends first along the B direction. Due to the deformation constraints of the plate itself and the heating movement direction, the contraction force P L along the plate's L direction lags behind P B . As shown in Figure 4b, after bending, deformation occurs along the B direction, the P L resultant force (T L ) is applied to the centroid of the B direction section, and a bending moment M L is created. Under M L , a deformation occurs along the plate's L direction that is opposite to the plate's B bending direction. This is why all of the shapes tested by the heating along the upper surface central line of the plate in the experiments are saddles.

Comparison between Experiment and Finite Element Method
Several sections and points in Figure 5 are selected to compare the temperature and deformation from the finite element calculation with the test results. The sections include the SL1-SL1 section, which coincides with the heating line, the SL2-SL2 section at the plate end, which is parallel to the heating line, the SB2-SB2 section at the plate end, which is vertically oriented to the heating line and the SB1-SB1 section at L/2. The point selected is point T1 at the plate's center.  Figure 6 compares the temperature variation from the finite element calculations with the test results at the plate's central point, T1, during heating. The diagram shows that based on the coil's dimensions, time record and speed, the relative position of the coil versus T1 at any moment can be derived. The finite element calculation results show that before 50 s, the temperature at T1 does not rise. Next, the temperature fluctuates in a small range and rises continuously until approximately 97 s. Thereafter, it declines steadily. The coil center passes T1 approximately 80 s after the beginning of the test. When the coil center and T1 coincide, the temperature at T1 is not at the highest level.

Comparison between Experiment and Finite Element Method
Several sections and points in Figure 5 are selected to compare the temperature and deformation from the finite element calculation with the test results. The sections include the S L1 -S L1 section, which coincides with the heating line, the S L2 -S L2 section at the plate end, which is parallel to the heating line, the S B2 -S B2 section at the plate end, which is vertically oriented to the heating line and the S B1 -S B1 section at L/2. The point selected is point T 1 at the plate's center.

Comparison between Experiment and Finite Element Method
Several sections and points in Figure 5 are selected to compare the temperature and deformation from the finite element calculation with the test results. The sections include the SL1-SL1 section, which coincides with the heating line, the SL2-SL2 section at the plate end, which is parallel to the heating line, the SB2-SB2 section at the plate end, which is vertically oriented to the heating line and the SB1-SB1 section at L/2. The point selected is point T1 at the plate's center.  The diagram shows that based on the coil's dimensions, time record and speed, the relative position of the coil versus T1 at any moment can be derived. The finite element calculation results show that before 50 s, the temperature at T1 does not rise. Next, the temperature fluctuates in a small range and rises continuously until approximately 97 s. Thereafter, it declines steadily. The coil center passes T1 approximately 80 s after the beginning of the test. When the coil center and T1 coincide, the temperature at T1 is not at the highest level.  Figure 6 compares the temperature variation from the finite element calculations with the test results at the plate's central point, T 1 , during heating. The diagram shows that based on the coil's dimensions, time record and speed, the relative position of the coil versus T 1 at any moment can be derived. The finite element calculation results show that before 50 s, the temperature at T 1 does not rise. Next, the temperature fluctuates in a small range and rises continuously until approximately 97 s. Thereafter, it declines steadily. The coil center passes T 1 approximately 80 s after the beginning of the test. When the coil center and T 1 coincide, the temperature at T 1 is not at the highest level.  The finite element calculation shows that the temperature at T1 fluctuates slightly before reaching its highest level. There are two reasons for this: the coil panel is not continuous. Before passing T1, there is a large amount of heat dissipation from the coil toward the unheated "cold plate" in the front. After the coil passes T1, the "cold plate" before T1 becomes a "hot plate", and the temperature at T1 declines steadily after a short period of fluctuation and increase. Additionally, because the temperature monitoring point at T1 is blocked by the moving coil near 80 s, the measurement data during this period are invalid. Because the temperature is measured at regular intervals (a discontinuous measurement method), small temperature fluctuations are not reflected. However, the finite element calculation results and the test data are closely related throughout the process. To further validate the finite element calculation method, data are collected from the temperature sensor C2 for comparison. The temperature variation versus time at C2 is the variation of the highest temperature at the plate heating line after 4 s (C2 is 20 mm from the coil edge, and the coil travel speed is 5 mm/s). The test results are compared with the finite element calculation and shown in Figure 7, which confirms that the two match closely. Figure 8 shows the heat distribution from the finite element model of heat transmission after heating for 115 s. The plate deformation shapes from the test and the finite element calculation are shown in Figure 9. Both results are saddle-shaped. Figure 10   The finite element calculation shows that the temperature at T 1 fluctuates slightly before reaching its highest level. There are two reasons for this: the coil panel is not continuous. Before passing T 1 , there is a large amount of heat dissipation from the coil toward the unheated "cold plate" in the front. After the coil passes T 1 , the "cold plate" before T 1 becomes a "hot plate", and the temperature at T 1 declines steadily after a short period of fluctuation and increase. Additionally, because the temperature monitoring point at T 1 is blocked by the moving coil near 80 s, the measurement data during this period are invalid. Because the temperature is measured at regular intervals (a discontinuous measurement method), small temperature fluctuations are not reflected. However, the finite element calculation results and the test data are closely related throughout the process. To further validate the finite element calculation method, data are collected from the temperature sensor C 2 for comparison. The temperature variation versus time at C 2 is the variation of the highest temperature at the plate heating line after 4 s (C 2 is 20 mm from the coil edge, and the coil travel speed is 5 mm/s). The test results are compared with the finite element calculation and shown in Figure 7, which confirms that the two match closely.  The finite element calculation shows that the temperature at T1 fluctuates slightly before reaching its highest level. There are two reasons for this: the coil panel is not continuous. Before passing T1, there is a large amount of heat dissipation from the coil toward the unheated "cold plate" in the front. After the coil passes T1, the "cold plate" before T1 becomes a "hot plate", and the temperature at T1 declines steadily after a short period of fluctuation and increase. Additionally, because the temperature monitoring point at T1 is blocked by the moving coil near 80 s, the measurement data during this period are invalid. Because the temperature is measured at regular intervals (a discontinuous measurement method), small temperature fluctuations are not reflected. However, the finite element calculation results and the test data are closely related throughout the process. To further validate the finite element calculation method, data are collected from the            These results show that the current finite element computing model and method can accurately simulate plate deformation under induction heating.

Effect of Coil Width during Forming
Once the applicability of the finite element computing method has been validated by the test results, the finite element method is employed to study the effect of coil dimensions on forming shape and processing efficiency by modifying the coil dimension and calculating the number of heating lines required to produce a specific deformation shape in the plate.
To facilitate discussion, a square plate with equal length and width is considered, i.e., L = B. The plate length is L = 1000 mm, and its width is B = 1000 mm. The plate thickness has 2 options: t = 16 mm or t = 20 mm. Additionally, the coil outer edge length and width are equal, i.e., LC = LB. The form of the coil's panel is chosen the same as in Figure 1a. The coil moves over the plate along the plate's central line, which is the same as the test. Table 3 lists calculation schemes for different coil widths. Since both the plate and coil are square in shape, to facilitate representation, the parameter that reflects the dimension ratio of the coil versus the plate is defined as the ratio of their widths, i.e., LC/B. Normally, the coil width is always less than the plate width. Therefore, LC/B is less than 1. Five conditions are calculated, and the maximum coil width is approximately 1/3 of the plate width. The highest temperature produced by the coil in the scheme is the highest acceptable temperature for a heated plate in the heating forming of a typical ship hull plate.  Figure 12 and Figure 13 show the plate deformations caused by line heating with coils of various sizes. In the diagrams, δB represents the maximum vertical deflection of the SB1-SB1 section in Figure  5, and δL represents the maximum vertical deflection of the SL1-SL1 section in Figure 5. Figure 12 and Figure 13 show that when the coil travel speed and highest temperature are fixed, within a large coil width variation range, the plate's maximum transversal and longitudinal deflections increase with the coil dimension. Thus, the plate deformation increases with the coil dimension. These results show that the current finite element computing model and method can accurately simulate plate deformation under induction heating.

Effect of Coil Width during Forming
Once the applicability of the finite element computing method has been validated by the test results, the finite element method is employed to study the effect of coil dimensions on forming shape and processing efficiency by modifying the coil dimension and calculating the number of heating lines required to produce a specific deformation shape in the plate.
To facilitate discussion, a square plate with equal length and width is considered, i.e., L = B. The plate length is L = 1000 mm, and its width is B = 1000 mm. The plate thickness has 2 options: t = 16 mm or t = 20 mm. Additionally, the coil outer edge length and width are equal, i.e., L C = L B . The form of the coil's panel is chosen the same as in Figure 1a. The coil moves over the plate along the plate's central line, which is the same as the test. Table 3 lists calculation schemes for different coil widths. Since both the plate and coil are square in shape, to facilitate representation, the parameter that reflects the dimension ratio of the coil versus the plate is defined as the ratio of their widths, i.e., L C /B. Normally, the coil width is always less than the plate width. Therefore, L C /B is less than 1. Five conditions are calculated, and the maximum coil width is approximately 1/3 of the plate width. The highest temperature produced by the coil in the scheme is the highest acceptable temperature for a heated plate in the heating forming of a typical ship hull plate.   Figures 12 and 13 show the plate deformations caused by line heating with coils of various sizes. In the diagrams, δ B represents the maximum vertical deflection of the S B1 -S B1 section in Figure 5, and δ L represents the maximum vertical deflection of the S L1 -S L1 section in Figure 5. Figures 12 and 13 show that when the coil travel speed and highest temperature are fixed, within a large coil width variation range, the plate's maximum transversal and longitudinal deflections increase with the coil dimension. Thus, the plate deformation increases with the coil dimension.  For plates with different thicknesses, the calculation results show similar patterns. The diagrams also show that when the coil dimension increases to a certain level, the increasing trend of transversal deflection gradually slows. For longitudinal deflection, when LC/B > 0.3 and as the coil dimension continuously increases, the bending deflection demonstrates a declining trend. This occurs because for the transversal deflection, the distance between the heating surface of the coil and the upper surface of the deformed plate increases as the coil width increases. Hence, although the temperature at the heating line of the plate is fixed in the calculation, the high-temperature effective range decreases as this distance increases. Therefore, the deflection increase rate slows. For longitudinal deflection, as shown in Figure 4, the distance from section TL to the B-direction section centroid decreases, which reduces the bending moment ML and thus reduces the deflection in the L direction. The result shows that when coil size increases to a certain level, it is possible that heating gradually causes changes in the local characteristics, which gradually weakens the local deformation characteristics of the plate.

Width Effect on Deformation
The calculated effects of the coil width on the plate curvature are shown in Figure 14. The diagrams show that as coil size increases, the transversal maximum curvatures and curvature ranges increase accordingly.  For plates with different thicknesses, the calculation results show similar patterns. The diagrams also show that when the coil dimension increases to a certain level, the increasing trend of transversal deflection gradually slows. For longitudinal deflection, when LC/B > 0.3 and as the coil dimension continuously increases, the bending deflection demonstrates a declining trend. This occurs because for the transversal deflection, the distance between the heating surface of the coil and the upper surface of the deformed plate increases as the coil width increases. Hence, although the temperature at the heating line of the plate is fixed in the calculation, the high-temperature effective range decreases as this distance increases. Therefore, the deflection increase rate slows. For longitudinal deflection, as shown in Figure 4, the distance from section TL to the B-direction section centroid decreases, which reduces the bending moment ML and thus reduces the deflection in the L direction. The result shows that when coil size increases to a certain level, it is possible that heating gradually causes changes in the local characteristics, which gradually weakens the local deformation characteristics of the plate.
The calculated effects of the coil width on the plate curvature are shown in Figure 14. The diagrams show that as coil size increases, the transversal maximum curvatures and curvature ranges increase accordingly. For plates with different thicknesses, the calculation results show similar patterns. The diagrams also show that when the coil dimension increases to a certain level, the increasing trend of transversal deflection gradually slows. For longitudinal deflection, when L C /B > 0.3 and as the coil dimension continuously increases, the bending deflection demonstrates a declining trend. This occurs because for the transversal deflection, the distance between the heating surface of the coil and the upper surface of the deformed plate increases as the coil width increases. Hence, although the temperature at the heating line of the plate is fixed in the calculation, the high-temperature effective range decreases as this distance increases. Therefore, the deflection increase rate slows. For longitudinal deflection, as shown in Figure 4, the distance from section T L to the B-direction section centroid decreases, which reduces the bending moment M L and thus reduces the deflection in the L direction. The result shows that when coil size increases to a certain level, it is possible that heating gradually causes changes in the local characteristics, which gradually weakens the local deformation characteristics of the plate.
The calculated effects of the coil width on the plate curvature are shown in Figure 14. The diagrams show that as coil size increases, the transversal maximum curvatures and curvature ranges increase accordingly. Appl. Sci. 2018, 8

Forming Capacity of a Wider Coil
The previous results show that increasing the coil width can produce a larger curvature. However, a wider coil could be unfavorable to produce shapes with smaller curvatures. In this study, the coil input power is changed to calculate and investigate the curvature coverage of a wider coil. The calculation is based on the coil used in Case 3. The plate deformation and curvature distribution under heating conditions with different input powers P are calculated, and the results are shown in Figure 15 and Figure 16.

Forming Capacity of a Wider Coil
The previous results show that increasing the coil width can produce a larger curvature. However, a wider coil could be unfavorable to produce shapes with smaller curvatures. In this study, the coil input power is changed to calculate and investigate the curvature coverage of a wider coil. The calculation is based on the coil used in Case 3. The plate deformation and curvature distribution under heating conditions with different input powers P are calculated, and the results are shown in Figures 15 and 16.

Forming Capacity of a Wider Coil
The previous results show that increasing the coil width can produce a larger curvature. However, a wider coil could be unfavorable to produce shapes with smaller curvatures. In this study, the coil input power is changed to calculate and investigate the curvature coverage of a wider coil. The calculation is based on the coil used in Case 3. The plate deformation and curvature distribution under heating conditions with different input powers P are calculated, and the results are shown in Figure 15 and Figure 16.

Forming Capacity of a Wider Coil
The previous results show that increasing the coil width can produce a larger curvature. However, a wider coil could be unfavorable to produce shapes with smaller curvatures. In this study, the coil input power is changed to calculate and investigate the curvature coverage of a wider coil. The calculation is based on the coil used in Case 3. The plate deformation and curvature distribution under heating conditions with different input powers P are calculated, and the results are shown in Figure 15 and Figure 16.   Figures 15 and 16 show that for a wider coil, changing the input power can produce deflection and curvature on a corresponding scale. For ship hull plates, the formation range of a wider coil satisfies the actual processing requirements.
In the test and previous calculation, the formed plates are mainly saddle-type. In order to verify the ability of a wider coil in forming other types, the heating patterns shown in Figure 17 are calculated and the highest temperature during heating is 700 • C. The deflection of the formed plate is shown in Figure 18. It can be seen from Figures 16 and 18 that a wider coil can form different curvatures and different types of a ship hull plate. This means that the capacity of the wider coil can meet the processing needs of the ship hull plates.  Figure 15 and Figure 16 show that for a wider coil, changing the input power can produce deflection and curvature on a corresponding scale. For ship hull plates, the formation range of a wider coil satisfies the actual processing requirements.
In the test and previous calculation, the formed plates are mainly saddle-type. In order to verify the ability of a wider coil in forming other types, the heating patterns shown in Figure 17 are calculated and the highest temperature during heating is 700 °C . The deflection of the formed plate is shown in Figure 18. It can be seen from Figure 16 and Figure 18 that a wider coil can form different curvatures and different types of a ship hull plate. This means that the capacity of the wider coil can meet the processing needs of the ship hull plates.

Efficiency Comparison of Different Coil Widths
In the following section, a forming deformation shape of the plate is selected to investigate the influence of the heating time with different coil widths. The calculations are based on the parallel heating of the coil in Case 5 (a narrower coil) along the plate's L direction as shown in Figure 19 and the single-pass heating of the coil in Case 3 (a wider coil) as shown in Figure 4. The two forming deformation shapes are then compared in order to study the forming shape and processing efficiency. In Case 5, the distance between the heating lines is W = 0.05 m. In both calculations, the highest temperature at the plate's heating line is fixed at 700 °C and the travel speeds at all heating lines are equal.  Figure 15 and Figure 16 show that for a wider coil, changing the input power can produce deflection and curvature on a corresponding scale. For ship hull plates, the formation range of a wider coil satisfies the actual processing requirements.
In the test and previous calculation, the formed plates are mainly saddle-type. In order to verify the ability of a wider coil in forming other types, the heating patterns shown in Figure 17 are calculated and the highest temperature during heating is 700 °C . The deflection of the formed plate is shown in Figure 18. It can be seen from Figure 16 and Figure 18 that a wider coil can form different curvatures and different types of a ship hull plate. This means that the capacity of the wider coil can meet the processing needs of the ship hull plates.

Efficiency Comparison of Different Coil Widths
In the following section, a forming deformation shape of the plate is selected to investigate the influence of the heating time with different coil widths. The calculations are based on the parallel heating of the coil in Case 5 (a narrower coil) along the plate's L direction as shown in Figure 19 and the single-pass heating of the coil in Case 3 (a wider coil) as shown in Figure 4. The two forming deformation shapes are then compared in order to study the forming shape and processing efficiency. In Case 5, the distance between the heating lines is W = 0.05 m. In both calculations, the highest temperature at the plate's heating line is fixed at 700 °C and the travel speeds at all heating lines are equal.

Efficiency Comparison of Different Coil Widths
In the following section, a forming deformation shape of the plate is selected to investigate the influence of the heating time with different coil widths. The calculations are based on the parallel heating of the coil in Case 5 (a narrower coil) along the plate's L direction as shown in Figure 19 and the single-pass heating of the coil in Case 3 (a wider coil) as shown in Figure 4. The two forming deformation shapes are then compared in order to study the forming shape and processing efficiency. In Case 5, the distance between the heating lines is W = 0.05 m. In both calculations, the highest temperature at the plate's heating line is fixed at 700 • C and the travel speeds at all heating lines are equal. Considering the interval between the heating processes in Case 5, i.e., when the plate is heated for a second time, the residual temperature could affect the final plate deformation shape. This also makes it difficult to compare the heating deformation time for Case 5 with that of Case 3. For parallel heating, different intervals are applied to the two heating lines for calculation; i.e., after the first heating line is completed, different intervals are applied before the second heating.  Figure 20 shows the final deflection at the plate B direction center for two heating lines subjected to parallel heating with different intervals. It shows that in parallel heating, the interval between the heating lines has an insignificant impact on the plate heating deformation. Hence, compared with heating completion time for Case 3, the parallel heating interval for Case 5 is zero in theory. This means that the processing time for Case 5 is twice that for Case 3. When the single-pass heating for Case 3 and the two-pass heating for Case 5 have the same travel speed and the same maximum temperature, the calculation results are as shown in Figure 21 and Figure 22. Considering the interval between the heating processes in Case 5, i.e., when the plate is heated for a second time, the residual temperature could affect the final plate deformation shape. This also makes it difficult to compare the heating deformation time for Case 5 with that of Case 3. For parallel heating, different intervals are applied to the two heating lines for calculation; i.e., after the first heating line is completed, different intervals are applied before the second heating. Figure 20 shows the final deflection at the plate B direction center for two heating lines subjected to parallel heating with different intervals. It shows that in parallel heating, the interval between the heating lines has an insignificant impact on the plate heating deformation. Hence, compared with heating completion time for Case 3, the parallel heating interval for Case 5 is zero in theory. This means that the processing time for Case 5 is twice that for Case 3. When the single-pass heating for Case 3 and the two-pass heating for Case 5 have the same travel speed and the same maximum temperature, the calculation results are as shown in Figures 21 and 22. Considering the interval between the heating processes in Case 5, i.e., when the plate is heated for a second time, the residual temperature could affect the final plate deformation shape. This also makes it difficult to compare the heating deformation time for Case 5 with that of Case 3. For parallel heating, different intervals are applied to the two heating lines for calculation; i.e., after the first heating line is completed, different intervals are applied before the second heating.  Figure 20 shows the final deflection at the plate B direction center for two heating lines subjected to parallel heating with different intervals. It shows that in parallel heating, the interval between the heating lines has an insignificant impact on the plate heating deformation. Hence, compared with heating completion time for Case 3, the parallel heating interval for Case 5 is zero in theory. This means that the processing time for Case 5 is twice that for Case 3. When the single-pass heating for Case 3 and the two-pass heating for Case 5 have the same travel speed and the same maximum temperature, the calculation results are as shown in Figure 21 and Figure 22.    shapes of the plate, Case 5 requires two-pass heating to achieve the same plate deformation shape as single-pass heating for Case 3, which means a higher forming processing efficiency for Case 3.
Based on the above calculation results, a moderate increase in coil width essentially increases the plate heating range and the local contraction force, which is favorable to increasing the deformation level of the processed plate. During heating, when the coil travel speed is fixed and for a specific plate shape, a wider coil requires less heating time than a narrower coil does. This means that a wider coil has a higher forming efficiency than a narrower one. Additionally, as the maximum temperature cannot increase infinitely, for a wider coil, the input power can be reduced to cover a narrower coil to produce a small deformation or small curvature. However, because an increase in power input results in a further increase in temperature, when the maximum temperature is constrained, it is difficult for a narrower coil to achieve a large deformation or a large curvature produced by a wider coil by increasing the input power of a narrower coil.
It is worth noting that an excessively wide coil could change the localized heating condition and reduce the local deformation of the heated plate. Therefore, the coil dimension selection should be optimized.    Figure 22 show comparisons of the deformation shapes at the plate transversal and longitudinal flexure lines of center sections. For the transversal and longitudinal deformation shapes of the plate, Case 5 requires two-pass heating to achieve the same plate deformation shape as single-pass heating for Case 3, which means a higher forming processing efficiency for Case 3.
Based on the above calculation results, a moderate increase in coil width essentially increases the plate heating range and the local contraction force, which is favorable to increasing the deformation level of the processed plate. During heating, when the coil travel speed is fixed and for a specific plate shape, a wider coil requires less heating time than a narrower coil does. This means that a wider coil has a higher forming efficiency than a narrower one. Additionally, as the maximum temperature cannot increase infinitely, for a wider coil, the input power can be reduced to cover a narrower coil to produce a small deformation or small curvature. However, because an increase in power input results in a further increase in temperature, when the maximum temperature is constrained, it is difficult for a narrower coil to achieve a large deformation or a large curvature produced by a wider coil by increasing the input power of a narrower coil.
It is worth noting that an excessively wide coil could change the localized heating condition and reduce the local deformation of the heated plate. Therefore, the coil dimension selection should be optimized. For the transversal and longitudinal deformation shapes of the plate, Case 5 requires two-pass heating to achieve the same plate deformation shape as single-pass heating for Case 3, which means a higher forming processing efficiency for Case 3.
Based on the above calculation results, a moderate increase in coil width essentially increases the plate heating range and the local contraction force, which is favorable to increasing the deformation level of the processed plate. During heating, when the coil travel speed is fixed and for a specific plate shape, a wider coil requires less heating time than a narrower coil does. This means that a wider coil has a higher forming efficiency than a narrower one. Additionally, as the maximum temperature cannot increase infinitely, for a wider coil, the input power can be reduced to cover a narrower coil to produce a small deformation or small curvature. However, because an increase in power input results in a further increase in temperature, when the maximum temperature is constrained, it is difficult for a narrower coil to achieve a large deformation or a large curvature produced by a wider coil by increasing the input power of a narrower coil.
It is worth noting that an excessively wide coil could change the localized heating condition and reduce the local deformation of the heated plate. Therefore, the coil dimension selection should be optimized.