3.1. Microstructural Characterization
Figure 2 shows the full thickness microstructure of the transverse section. By comparing the microstructure of different C content, it can be seen that there are significant differences in the distribution of microstructure along the thickness direction and the grain size of ELC is slightly smaller than that of LC. The microstructure in the thickness direction of strip is non-uniform, the grain size distribution of ELC has five-layer structure, while that of LC has only three-layer structure. In
Figure 2a the microstructure of ELC from the upper surface to the lower surface along the thickness direction includes an upper surface coarse grain area with a thickness of about 83.0 µm and an average grain size of 20.0 µm, a near upper surface fine grain area with a thickness of about 83.7 µm and an average grain size of 7.4 µm, a central medium grain area with a grain size of about 10.8 µm, a near lower surface fine grain area with a thickness of about 90.4 µm and an average grain size of 7.6 µm, and an lower surface coarse grain area with the thickness is about 85.5 µm and the average grain size is 17.5 µm. In
Figure 2b the microstructure of LC includes an upper surface fine grain area with a thickness of about 159.6 µm and an average grain size of 7.1 µm, a central medium grain area with a grain size of about 10.3 µm, and an upper surface fine grain area with the thickness is about 162.4 µm and the average grain size is 6.8 µm.
In order to further observe the difference of microstructure between ELC and LC, the SEM microstructures exhibited in
Figure 3, consist of the ferrite and a few cementite distributed at ferrite grain boundaries or corners. In
Figure 3a the microstructure of ELC includes an upper surface coarse grain area with a thickness of about 83.5 µm and an average grain size of 20.3 µm, and a near upper surface fine grain area with a thickness of about 81.7 µm and an average grain size of 7.2 µm. In
Figure 3b the microstructure of LC includes an upper surface fine grain area with a thickness of about 159.6 µm and an average grain size of 7.1 µm. In
Figure 3c,d the microstructure of ELC and LC is a medium grain area with average grain sizes of 10.6 µm and 10.2 µm, respectively. In
Figure 3e the microstructure of ELC includes a lower surface coarse grain area with a thickness of about 83.9 µm and an average grain size of 20.3 µm, and a near upper surface fine grain area with a thickness of about 94.3 µm and an average grain size of 7.5 µm. In
Figure 3f, the microstructure of LC includes an upper surface fine grain area with a thickness of about 157.0 µm and an average grain size of 6.9 µm. Compared with
Figure 2, it can be seen that there is little difference in grain size and area thickness, which is mainly related to the magnification and the clarity of grain boundary.
3.2. Characteristics of Cementite and Precipitates
According to the Fe-Fe
3C phase diagram, ELC and LC are located on the left and right sides of point P (maximum dissolved carbon content in α-Fe) respectively due to different carbon content, and their microstructure and phase content will be significantly different. When ELC and LC are slowly cooled from 727 °C to room temperature, because less than 0.0008% C can be dissolved in ferrite at room temperature, excess carbon will precipitate along the ferrite grain boundaries in the form of cementite, which is called Fe
3C
III. Similarly, carbon content higher than 0.0218% will undergo eutectoid transformation to form the microstructure of ferrite (α-Fe) and pearlite (P), therefore, in theory, α-Fe, P and Fe
3C
III can be observed in LC at room temperature. According to the lever law [
10],
Here, ɷ(A) is the relative quantity of component A, xa, xb and xp are the fraction of component A, B and alloy P, respectively.
for ELC: ɷ(Fe3CIII) = (0.012 − 0.0008)/(6.69 − 0.0008) = 0.17%.
for LC: ɷ(Fe3CIII) = (0.0218 − 0.0008)/(6.69 − 0.0008) = 0.31%,
ɷ(P) = (0.044 − 0.0218)/(0.77 − 0.0218) = 2.97%.
It can be seen from
Figure 4 that there are significant differences in the distribution and morphology of cementite for ELC and LC. In
Figure 4a, the microstructure of ELC consists of dispersed ferrite and a small amount of Fe
3C
III (see red rectangulars in
Figure 4a). Fe
3C
III in the form of short rod (
Figure 4b) and irregularly shape (
Figure 4c) are mainly distributed at the boundaries and corners of ferrite. At the same time, there are many nano precipitates in the ferrite (
Figure 4c). In
Figure 4d, the microstructure of LC consists of dispersed ferrite and a small amount of pearlite (see red ovals in
Figure 4d), cementite in cluster pearlite located at the corner of ferrite exists in different pearlite fields in uniform lamellar form (
Figure 4e) and cementite in uniform lamellar form is distributed at the ferrite grain boundaries (
Figure 4f), similarly, a small number of spherical precipitates exist in the ferrite (
Figure 4d,f).
After the steel strips were corroded by the aqueous solution mixed with 10 g/L ammonium sulfate and 10 g/L citric acid, the particle size of precipitated particles obtained by filtration of the solution was analyzed by SAXS. The mass fraction distribution and mass density distribution under different particle sizes are obtained by SAXS, as shown in
Figure 5. The mass fraction of less than 36 nm and >200 nm in ELC is greater than that of in LC, and the mass fraction of 36–200 nm is vice versa. The mass fraction is over 35% in 140–200 nm, the mean size of ELC is 136.3 nm, which is slightly more than 131.4 nm of LC, mainly because the mass fraction above 200 nm in ELC is 118% more than that in LC (
Figure 5a). The mass density distribution has the same law as the mass fraction distribution, and the highest mass density is between 1–5 nm.
Relevant studies show that nanoscale oxide and sulfide precipitates had been observed in low carbon steel strips produced by CSP, and these small precipitates may contribute to the strengthening and grain refinement under certain conditions [
11]. In low-carbon aluminum-killed steel, the second-phase particles frequently discovered are MnS, Al
2O
3, Fe
3C and AlN [
12,
13]. The morphology and distribution of precipitates observed under TEM after carbon extraction replicas of ultra-thin strip produced by ESP are shown in
Figure 6. It can be seen from the comparison that the precipitates of ELC are large in quantity and small in size, mainly square AlN, spherical Fe
3C and Al
2O
3 (
Figure 6a), while the precipitates of LC are small in quantity but large in size, mainly large size ellipsoidal MnS and rectangular AlN, in addition, lamellar pearlite with a length of 4.36 µm is observed at the corner of ferrite boundaries (
Figure 6b). The result is consistent with
Figure 5.
3.3. Characteristics of Mechanical Properties
The engineering stress-strain curves and tensile properties of the two steels in rolling directions (0°) and transverse directions (90°) are shown in
Figure 7. The initial yielding exhibits a material instability known as Lüders banding, which is a dislocation driven phenomenon that macroscopically manifests as inhomogeneous deformation. It exhibits an initial shape stress peak (upper yield stress) followed by a stress plateau (lower yield stress) that extends over a Lüders strain, it is called the discontinuous yield phenomenon. It can be seen that the upper yield strength (Re
H) (see orange rectangular in
Figure 7) of LC is more than 40 MPa higher than the tensile strength (Rm), while that of ELC is only higher than 5 MPa. Rm at 0° is about 5 MPa lower than Rm at 90°, the lower yield strength (Re
L) at 0° is about 10 MPa lower than Re
L at 90°. Each yield platform has obvious zigzag shape and the percentage yield point extension (see purple oval in
Figure 7) or Lüders strain is about 10%, but the percentage yield point extension of low carbon steel produced by compact endless casting and rolling process is only 5% [
14]. The elongation (A) at 0° is higher than A at 90°, in particular, A at 90° of ELC decreases significantly mainly because the percentage yield point extension reduced by 3%, which needs further study. On the whole, the strength other than Re
H of ELC is about 20 MPa lower than that of LC and A of ELC is lower than that of LC. The longer yield platform of ESP steel strip is conducive to improve the elongation of the material and enhance the plasticity, but it also shows that the steel has room temperature aging and is not conducive to stamping forming [
15]. Therefore, it is necessary to study the generation mechanism of yield platform and high Re
H and their influence on forming properties.
In order to test the stamping performance of steel strip, plastic strain ratio (r), weight average of r values (
) and degree of planar anisotropy (Δr) are usually used to measure the degree of anisotropy [
16]. The r value and
are required as high as possible, and Δr as small as possible.
Table 3 shows r value and n value for 1.0 mm thickness. It can be seen that r values deviating from rolling direction by 0° (r0), 45° (r45) and 90° (r90), and
value of ELC higher than that of LC, but |Δr| of ELC is relatively small, indicating that the ear making is small, that is, the anisotropy of ELC is smaller than that of LC. In addition, the Δr < 0 of the two steels indicates that the ear appears in the direction of 45° to the rolling direction. The n values of the two steels are similar, near 0.22, and the n value of rolling direction is slightly higher than that of transverse direction.
3.4. Characteristics of Internal Friction Peaks
Because the Snoek relaxation can be used to study the distribution and variation characteristics of C and N atoms in the octahedral gap of ferrite, the internal friction method for measuring Snoek relaxation is a common analytical method for measuring the content of solid solution carbon atoms in iron and steel [
17]. The internal frictions—temperature spectrums of ultra-thin hot rolled strip produced by ESP—are shown in
Figure 8.
is total internal friction measured by internal friction meter,
is the real internal friction obtained by calculation,
is the background internal friction deducted by the calculation software attached to the equipment, and the relationship between them is
=
+
. Then, the peaks of
were separated and fitted by OriginPro 8.5. It can be seen from
Figure 8 that the real internal friction is composed of three internal friction peaks (P1, P2 and P3) and the peak value increases significantly with the increase of temperature. The peak temperatures of P1, P2 and P3 are about 20 °C, 40 °C and 70 °C, respectively. At the same time, the P2 peak shape and half width of LC are more obvious than those of LC. It can be inferred that there is an internal friction peak above 120 °C because the internal friction increases gradually when the temperature is higher than 100 °C. Relevant studies show that the Snoek peak of solid solution nitrogen atoms appears at about 20 °C [
18,
19], the Snoek peak of solid solution carbon atoms appears about 40 °C [
19,
20,
21,
22,
23] or about 67 °C [
15,
20,
24] and the activation energy is about 84 kJ/mol. In SDH3 steel, it is found [
25] that the Snoek peak of solid solution carbon atoms is decomposed into two peaks, s1 and s2. The s1 peak is the Snoek peak of solid solution carbon atoms in pure α-Fe, and s2 peak is the Snoek peak of solid solution carbon atoms in body centered cubic lattice in which some Fe atoms are replaced by weak carbide forming elements such as Si and Mn. It is also found [
20] that the internal friction spectrum of automotive plates with different stamping properties has obviously different characteristics with different peak numbers. According to these results, it can be preliminarily determined that the peak near 20 °C is the Snoek peak of solid solution nitrogen atoms, and the other two peaks are the Snoek peak of solid solution carbon atoms.
In the binary Fe-C alloy, the height of the Snoek peak (
) is assumed to be directly proportional to the solid solution atonic content ([C]) [
24]. That is,
Here, K is a factor which depends on the grain size, substitutional alloying element and the texture of the alloy. In this experiment, K is recommended to be 1.33 for solid solution carbon atoms and 1.28 for solid solution nitrogen atoms, this value is similar to that in other literatures [
26,
27]. The solid solution carbon atom content of ELC at P3 is significantly higher than that of LC. The reason is that the long of layer cooling line in ESP is about 40 m and that in the conventional hot rolling line is about 120 m. Therefore, high cooling speed results in supersaturated solution of carbon atoms in ultra-thin strip steel. It is considered that there are two reasons why the content of solid solution carbon atoms in ELC is higher than that in LC. One is that LC undergoes eutectoid transformation to form pearlite, the carbon atoms dissolved in or near the pearlite field are easy to diffuse to the lamellar cementite and precipitate in the form of Fe
3C
III because of the short distance. The other is that the ferrite grains of LC are relatively small, and the content of dissolved carbon in ferrite is nearly twice that of ELC, so these solid solution carbons are also easier to diffuse to the ferrite grain boundary and precipitate in the form of Fe
3C
III or take heterogeneous points as the nucleation core to precipitate spherical cementite in ferrite grains, as shown in
Figure 4. The activation energy (H) can be calculated [
28] by:
where R is the ideal gas constant and R = 8.314472 J/(mol·K), Tm and fm correspond to the internal friction and frequency of the peak, k is Boltzmann constant and k = 1.3806505 × 10
−23 J/K, h is the Planck constant and h = 6.62607015 × 10
−34 J·s, Δs is the activation entropy and Δs = 1.1 × 10
−4 eV/K.
Table 4 shows the important indexes characterizing the internal friction peaks for 1.0 mm thickness. It can be seen that the content of solid solution nitrogen atoms in P1 peak is lower than 2 ppm, which is mainly due to the high Al (≥0.035%) and low N (≤60 ppm) in the steel (
Table 1) and precipitation in the form of AlN (
Figure 6), resulting in basically no free nitrogen atoms in the steel. The solid solution carbon atom and activation energy of P2 peak are lower than those of P3. The activation energy of P3 peak is in the range of 0.84 ± 0.03 eV [
29] and 0.76–0.89 eV [
25], so therefore, it is certain that the P3 peak is the carbon snoek peak of α-Fe and the P2 peak is the carbon Snoek peak of body centered cubic lattice in which part of Fe is replaced by Si and Mn.
3.6. Texture Analysis by EBSD
Although the texture was analyzed macroscopically by XRD, EBSD analysis was carried out along the thickness direction in order to obtain more detailed information about grain orientation. The IPF of main texture component for ELC and LC is shown in
Figure 11, It can be seen that the density of {111}, {211} and {001} parallel to the rolling direction (X0) in ELC is higher than that in LC, the density of {111}, {211} and {001} parallel to RD (X0) in ELC is higher than that in LC, the density of {110} parallel to ND (Y0) in ELC is higher than that in LC, and the density of {111} and {332} parallel to TD (Z0) in ELC is higher than that in LC. The change trend is similar to that in
Figure 10.
ND fiber texture distribution and fraction of orientation deviation from {111} <uvw> with 20° for ELC and LC is shown in
Figure 12. It can be seen that the grain distribution is similar to that in
Figure 2 and
Figure 3 and the {111} components account for approximately 28.4% for ELC, while this ratio only reaches 16.9% for LC. At the same time, it can also be seen that there are more {111} components account in the fine grain layer of ELC compared with other positions. The stamping formability of IF steel for automobile plate mainly depends on the r value, that is to say, it is better to have more favorable texture components, such as the γ texture ({111}//ND) [
31]. Therefore, it can be inferred that the stamping formability of ELC is better than that of LC.
The misorientation distribution of ultra-thin hot rolled strip for 1.0 mm thickness is shown in
Figure 13. Both ELC and LC show the characteristics of random misorientation distribution, but there are significant differences (see black oval in
Figure 13). The relative frequency of small angle grain boundary (<10°), especially sub grain boundary (<3°) and 60° of ELC is significantly lower than that of LC, while the relative frequency of 30–40° and about 52° is higher. The increase of small angle grain boundary indicates the increase of dislocation, deformation and strength, the increase of large angle grain boundary indicates high recrystallization. Therefore, it can be seen that there are regions with large deformation degree and regions with high recrystallization degree in ELC and LC, which may be related to the microstructure in
Figure 2.
The geometrically necessary dislocations density (ρ
GND) can be calculated from the local misorientation (θ) using the EBSD orientation data according to the strain gradient theory [
32], that is,
where, Δθ is weighted average of θ, b is burgers vector of α-Fe, u is the scanning step, in our experiment, b = 850 μm. The calculated dislocation density of ELC and LC are 8.21 × 10
13/m
2 and 9.55 × 10
13/m
2 respectively, it is confirmed that the dislocation density of ELC is lower than that of LC. The relevant research showed that the dislocation density of the hot rolled LC steel sheet (0.05% C) by CSP was 2.80 × 10
13/m
2 [
33].
In order to further explain the difference of dislocation density of ultra-thin strips, the dislocation was observed by TEM.
Figure 14 shows the dislocation structure for 1.0 mm thickness ultra-thin strip with different carbon content. The dislocation structure is uneven, according to the stress situation, it is considered that there are many dislocations in the pre-eutectoid ferrite grains, while there are few dislocations in the recrystallized ferrite or the eutectoid ferrite. ELC has many pinning points, dislocation lines and a few dislocation entanglements in
Figure 14a, but LC has many pinning points, dislocation lines and a few dislocation cells in
Figure 14b. It can be clearly seen from
Figure 14b that there are a large number of parallel dislocations in the ferrite grains, and the dislocation pinning points are rows of micro precipitates. The dislocation density of LC is higher than that of ELC, which is also one of the reasons why LC has higher upper yield strength than that of ELC. At the same time, a small amount of Fe
3C (
Figure 14a) and (FeMn)
3C (
Figure 14b) are found at the ferrite grain boundaries.
The sheet metal formability is mainly tested by earing test, Hole expanding test and V-shaped bending test. It is considered [
34] that the long yield platform is prone to wrinkles on the steel surface in the process of stamping or bending deformation, which affects the forming effect and appearance. Therefore, the formability of ultra-thin strip by ESP was tested.
Figure 15 shows the photograph of draw cups and earing heights at varied angels from rolling direction. It is shown that the ears of ELC were smaller than those of LC, there are four ears produced during drawing and their earing direction was 45°, and there are no obvious defects such as wrinkles, localized bands of plastic deformation on the appearance of the draw cups.
Several important indexes to characterize the earing propensity are listed in
Table 5 in which
t,
v,
e, Δhmax, and Ze meant the average height of ear peak, ear valley, earing, maximum ear height, and earing coefficient, respectively. Although Ze of both meets the user’s requirements of less than 5%, but,
t,
e, Δhmax, and Ze of ELC were lower than those of LC, so ELC has better earing performance than LC.
The morphology after hole expanded for ELC and LC is shown in
Figure 16. It can be seen that the hole diameter of ELC was larger than that of LC, and two small cracks appeared in ELC, while a large crack appeared in LC, which were a typical β fractures exceeding their elongation. The calculated limiting hole expansion ratio are 79.1% and 61.4% respectively, both meet the delivery requirement of more than 50%.
Figure 17 shows the V-shaped bending process and bending parts. The downward speed of the upper mold was 1 mm/s, holding for 30 s after reaching the specified position, and then the upper mold rises quickly, remove the sample and measure its angle. The measured angles were all 60° and the samples under different bending radium (1.5 mm, 3.0 mm, 6.0 mm) did not rebound, as shown in
Figure 17d, and there were no obvious defects such as wrinkles on the appearance of the bended parts.
From the above experimental results, it can be considered that the 1.0 mm ultra-thin hot rolled steel strip by ESP has good earing behavior, hole expansion ratio and bending performance, can meet the requirements of tropical cooling, is conducive to energy conservation and emission reduction, and achieves carbon neutralization as soon as possible.