In DSIF, a flexible support tool is used, which can change its position regarding the master tool. Based on this flexibility, many tool configurations are derived. The two tool configurations based on local support to the master tools are: aligned (DSIF-A) and normal (DSIF-LN) (
Figure 4a). In DSIF-A, the tool axes are parallel and on the same line. In the DSIF-LN configuration, the tool-tip centers are along the local normal at the contact point of the sheet [
23]. Due to the support tool’s ineffective utilization at the component opening, the DSIF-A configuration is not frequently used. Therefore, in this work, DSIF-L will refer to DSIF-LN unless otherwise specified. Two other tool configurations based on the support tool locations are DSIF-L and DSIF-P (
Figure 4a,b). In DSIF-P, the support tool moves at the part opening to act as a backing plate. It does not take part in the actual forming operation [
24]. The support tool coordinates remain fixed at the initial contour, whereas the master tool coordinates are according to the part profile. In ADSIF, Equations (1) and (2) can acquire the support tool coordinates. However, in most cases in the previous studies, the support tool position is determined based on adjusting the parameters
D and
S
values iteratively with respect to the master tool (
Figure 4c) [
21,
25].
Due to DSIF process flexibility, new toolpaths such as mixed-DSIF (MDSIF), multi-stage DSIF, and hybrid DSIF were derived. MDSIF is the combination of ADSIF and DSIF. In multi-stage, the components are formed in several stages. Hybrid DSIF (where the heat source is also incorporated) is executed for geometric accuracy and formability improvement of hard-to-form metals. In a nutshell, the flexible DSIF process can use different toolpath strategies to form components.
2.2. The Role of Thickness Variations in DSIF Toolpath
In ISF, the final sheet thickness is usually calculated by sine law, (tf=to⋅sin(90−θ)) where tf: the final sheet thickness after deformation, to: the original sheet thickness, and θ: local wall angle. The local wall angle can be used to find the thickness at any point in the component of complex geometry. The ti (instant sheet thickness) in Figure 3b is not necessarily the sheet thickness predicted by sine law. This difference in ti from the sheet thickness indicated by sine law at different forming heights affects the support tool–sheet contacts. It is due to differences in calculated and actual D and S values. Malhotra et al. [26] initially reported this shortcoming in the sine law while forming the 65° cone. Sine law was used to regulate the gap between the tools. After a certain forming height, the support tool disengaged from the sheet. The process degenerated to SPIF, resulting in early fracture. Squeezing was utilized to improve the support tool–sheet contact; however, it did not ensure accuracy.
According to Moser et al. [
27], successfully maintaining contact between tools and the sheet can improve sheet thickness distribution, increase material formability, and reduce the early fracture. In their view, factors responsible for the tool–sheet contact lost problem were an inaccurate prediction of thickness predicted by sine law, tool misalignment, and ignoring machine compliance effect. They concentrated on sheet thickness problems in their work and the spring back and machine compliance for the shamrock section with a 65° wall angle. Preliminary work in LS-DYNA determined the thickness profile. The
D and
S adjustments were according to the projected thickness of the sheet. The sheet thickness distribution was decoupled from wall angle and was associated with in-plane curvature and part height. The gap determined by sine law leads to disengagement of support tools, whereas the new approach works effectively. However, their work was specific to the shamrock part. For 90° wall angle, the sheet thickness becomes zero according to the sine law. Moser et al. [
28] modified the sine law for the vertical wall angle component to prevent the tool gap from approaching zero.
Otsu et al. [
29] compared the sheet thickness distribution for SPIF and DSIF-L. SPIF does not observe the sheet thickness variation at the part opening due to global bending effects. In DSIF, the variation in sheet thickness is started from the beginning (
Figure 5). It was attributed to the strong restraint on the sheet by the tools from both sides. The wall thickness predicted by sine law was 0.32 mm. As evident from
Figure 5, the thickness acquired with DSIF-L is relatively closer to the sine law prediction along the complete section; however, it does not match the thickness predicted by the sine law.
Bin Lu et al. [
30] compared the DSIF-L and DSIF-P strategies for wall thickness variation in a 0.5 mm sheet. No significant difference was observed in the sheet thickness acquired with DSIF-P (0.463 mm) and DSIF-L (0.461 mm). The slight difference for the DSIF-L, being on the lower side, was attributed to the local squeezing of the sheet. Malhotra et al. [
31] compared the ADSIF and SPIF and observed that the sheet thickness acquired with ADSIF was on the lower side. The sheet thickness variation is minimum across the complete part height compared to SPIF. Zhang et al. [
32] compared the sheet thickness variation in DSIF-L, ADSIF, and MDSIF. The thickness profile of the DSIF-L deviates relatively more from the sine law prediction, whereas the ADSIF and MDSIF processes were reported to be closer to the sine law curve.
The sheet thickness variation is the main study in SPIF [
33,
34,
35,
36]. In DSIF, the sheet thickness variation is relatively better than in SPIF; however, the unpredicted thickness variation leads to ineffective tool–sheet contact, which degenerates the process to SPIF. Formability and deformation can be improved by avoiding support tool–sheet lost contact.
2.3. Deformation and Fracture Mechanism in DSIF
Because of the increased compressive force provided by the support tool, it is usually assumed that the DSIF has higher formability than the SPIF. The support tool must maintain constant contact with the sheet to benefit from the compressive force. Meier et al. [
37] utilized the support tool with 300 N force in the DSIF-L orientation to ensure the support tool–sheet contact and reported a wall angle of 72° for the hyperboloid component. An earlier study in SPIF could not acquire a wall angle of more than 65°. The support tool force helped in increasing the formability by 12.5%. According to Malhotra et al. [
26], the DSIF toolpath improves precision and formability by stabilizing distortion within a narrow zone surrounding the tool’s contact site. B. Lu et al. [
38] observed the evolution of fracture depth in AA7075-T6 with varying squeezing forces. For squeezing force less than 240 N, there is no significant change in the fracture depth, and the tool squeezing does not make any apparent effect. Squeezing force from 240 to 480 N increases the formability from 20 to 30 mm. Increasing the squeezing force to 560 N harms the fracture depth (
Figure 6). It was analytically proved by a sudden drop in stress triaxiality point for stresses in the 240–480 N range. As illustrated in
Figure 7, the forces in this range were observed for various support tool adjustments (without tool shifting is DSIF-L orientation, whereas with tool shift is support tool adjustment in the middle position between DSIF-L and DSIF-A). The increasing squeezing force with tool shift adjustments positively impacts formability improvement than the other tool adjustments. The fracture occurred in both cases in the sheet region, which was in contact with a master tool, emphasizing the relevance of the support tool in delaying the fracture. Under excessive-high contact pressure and high friction, the tools may “clamp” and “stretch” the sheet in the moving direction, leading to high tensile stress conditions around the deformation zone and early failure of the sheet.
Valoppi et al. [
39] utilized the analytical model proposed by B. Lu et al. [
38] to investigate the fracture characteristics of Ti6Al4V sheets in the electric-assisted DSIF (E-DSIF) process. The deformation region was divided into three zones (Region-I, II, and III) to investigate the relationship between the E-DSIF fracture surfaces and the stress state (
Figure 8). Region-I and III experience meridional tensile stresses, and Region-II experience compressive stresses due to support tool squeezing. They reported that the outer Region-III is more susceptible to fracture due to reduced radial thickness, local bending, and more circumferential stress due to tool movement in that direction. It was further exaggerated by current, which increased through the thickness-shear too.
Zhang et al. [
40] analyzed the strain evolution for clover flange (
Figure 9). Increased circumferential and reduced meridional strain improved formability in stretch flanging. Meridional tensile and the localized deformation mode improved the formability of shrink flanging. With meridional tensile and circumferential compressive, the risk of wrinkling is minimized. With this combination, the strain state was close to pure shear, which was stable for sheet metal forming. Moser et al. [
41] investigated the shrink and a stretch portion of the shamrock part. The shrink portion experiences a mixture of negative strain (compressive force) and stretching. It resulted in an enlarged contact region of the support tool with the sheet, which helped effective tool–sheet contact. The support tool–sheet contact was not intact in the stretch flange as the formed height increased. It leads to a loss in squeezing, and the process becomes degenerated to SPIF having less geometric precision and formability.
In ADSIF, local bending of the sheet around the tool, a squeezing action due to the support tool, and shear perpendicular to and parallel to the tool motion improved formability [
20]. Malhotra et al. [
42] have shown that raising hydrostatic pressure and increasing through-the-thickness shear reduces the potential for sheet metal to fracture during the forming process. The higher hydrostatic pressure in ADSIF due to the support tool’s effective contact with the sheet prevents shear bands from forming. If shear bands do form, the compressive load state stops voids from expanding further, preventing material fracture. Davarpanah et al. [
43] hypothesized that the support tool’s continuous contact with the sheet improved formability.
In a nutshell, the successful contact of the support tool with the sheet increases the formability and delays the fracture, as evident in the previous studies. The unpredicted thickness variation during the DSIF process, on the other hand, leads to incorrect tool gap adjustment, which in most cases degenerates the DSIF to SPIF and early fracture. It has relation to component geometric precision and is examined in the next section.
3. Accuracy Improvement in DSIF Process
The required and form profile difference is considered a geometric error [
44]. In most cases, the required geometric accuracy for commercial parts is ±1 mm. In some cases, it becomes much stricter up to ±0.2 mm. The reported accuracy in ISF is still struggling to achieve these values [
16]. There are mainly three regions where a geometric error occurs in the form part: (a) sheet bending between the sheet support at the periphery and current tool position (b) in-accuracy at the wall region: The error source in this region is due to (i) tool and machine compliance (ii) in-process springback (iii) post-springback after part un-clamping from the fixture. These errors are considered a challenge, and researchers have utilized different techniques to overcome the root cause of these errors (c). The unwanted curvature at the final product base (the pillow effect) is seen below (
Figure 10).
Cone, pyramid, and funnel are some of the benchmark shapes trialed by researchers in ISF (Figure 11). Besides, based on the specific challenge, some researchers have worked on other profiles such as fish fin, shamrock, ellipsoidal, etc. For pyramid, length and width at the part opening are the same unless otherwise specified. Therefore, in (Table 1, Table 2 and Table 3), in the part size column, O is used to represent both the length and width of the pyramid, whereas, for cone and funnel, it is the diameter. In the funnel, the wall angle changes continuously. It is minimum at the part opening and increases along with the part height. The part errors in this study, in most cases, represent the under-forming part. Errors defined with the plus-minus sign are for over and under-forming parts.
The main focus of the early research was to validate the process’s capability to form complex parts. A robot having a 15 kg payload capacity was utilized by Meier et al. [
24] to form a cone from the AA 99.5 sheet. The formed part in some regions was undersized due to material springback and oversized in others due to the machine compliance. The part accuracy became homogeneous with the heavy-duty (360 kg payload capacity) robot, as the machine compliances were reduced. Wang et al. [
45] formed a complex part having curvature on both sides of the sheet without changing the setup. The machine used was a milling machine. SPIF and DSIF processes were compared for geometric accuracy by forming a sphere on the same blank. DSIF enhanced the accuracy at the part lower region, whereas SPIF performed better at the part opening area than DSIF. The reason was that a sphere was formed first with DSIF, which increased the sheet stiffness. SPIF took advantage of this increase in sheet stiffness for precision improvement at the component opening. Due to the C-frame structure utilized in their work, they were able to form parts with the wall angles in a certain range. While studying the effect of the tool gap for formability enhancement, Wang et al. [
46] recommended 0.8–0.9 times the thickness of the original sheet. The machine used was a lathe machine, which can mainly be used for symmetric shapes. Based on these preliminary works, DSIF comes to attention due to its adaptability with a different setup and complex part flexibly forming capability.