Experimental Investigation and Numerical Simulation of theCorrelation of Recovery and Texture in Bcc Metals and Alloys

  • Raabe D
  • Roters F
  • Marx V
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Abstract

Depending on the strain and temperature regime examined recovery of bcc metals during hot rolling or annealing subsequent to cold deformation often leads to the preservation of certain deformation texture components. A broad variety of mesoscopic and macroscopic texture data from both hot rolled and cold rolled and annealed bcc metals (Fe, Ta, Mo, Nb) and alloys (low‐carbon steels, ferritic stainless steels, transformer steels) is re‐examined with respect to such phenomena. The data suggest that two conditions promote strong recovery of certain bcc deformation texture components (e.g. {001} <110>), namely, the absence of kinetic instabilities, and the absence of thermodynamic and mechanic instabilities. The first case applies if the grains do not tend to generate large local misorientations in their interiors during plastic deformation. The second case applies if the stored dislocation density is low. Both features depend on the grain orientation. The experimental observations are complemented by three types of numerical simulations. The influence of the number of Burgers vectors equally involved during preceding deformation on the kinetics of static recovery is numerically studied using 2 dimensional dislocation dynamics. The orientation dependent inclination to generate local misorientations in the grain interiors is simulated using a Taylor type approach with different constraints on either side of the grain. The influence of the orientation dependence of recovery on the final annealing texture is simulated using a 3 dimensional cellular automation. Experiment and simulation show that both the recovery kinetics and the tendency to form kinetic instabilities considerably depend on the orientation. The latter effect seems to be essential for the prevalence of either RX or RC.

Figures

  • Table 1 Chemical composition of some alloys which are discussed in greater detail (alloy content is given in mass%).
  • Figure 2 Microstrucmre of a hot rolled ferritic stainless steel with 16.6mass% Cr (Figure 1, Table 1). a) Center layer (s 0) containing elongated flat grains, b) Sub-surface layer (s 0.8) containing both finely recrystallized (arrow A) and elongated recovered grains. Some elongated grains reveal a heavily sheared shape (arrow B).
  • Figure 3 Simulation of the profile of equivalent shear through the sheet thickness of a hot rolled steel sheet (Beynon et al. 1987).
  • Figure 4 Profile of the orientation density of the {001 < 110 > and of the Goss component through the hot band thickness of various ferritic stainless steels with 17mass% Cr content.
  • Figure 5 Influence of C, Si and Cr on the orientation density of {001} < 110 > in the center layer of hot rolled and 90% cold rolled samples. The open symbols indicate hot rolled band (HB) and the filled ones cold rolled band (90%).
  • Figure 6 Texture in the center layer of a hot rolled ferritic stainless steel with 17mass% Cr content (Raabe and Ylitalo 1995) a) Texture as determined by use of X-ray diffraction (four incomplete pole figures), b) Texture of the flat elongated recovered grains as selectively determined by use of EBSD.
  • Figure 7 Texture in the center layer of a 90% cold rolled and annealed low carbon steel (7 s, 1000 K, salt bath), (Raabe 1995) a) Texture as determined by use of X-ray diffraction (four incomplete pole figures), b) Texture of the unrecrystallized grains as selectively determined by use of EBSD (arrow in Figure 8).
  • Figure 8 Flat sections of the 90% cold rolled and annealed (7 s, 1000 K, salt bath) low carbon steel sheet the texture of which was shown in Figure 7. Figure 7b shows the texture of the recovered grains (arrow).

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APA

Raabe, D., Roters, F., & Marx, V. (1996). Experimental Investigation and Numerical Simulation of theCorrelation of Recovery and Texture in Bcc Metals and Alloys. Texture, Stress, and Microstructure, 26(1), 611–635. https://doi.org/10.1155/tsm.26-27.611

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