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Acta Metall Sin  2026, Vol. 62 Issue (9): 1487-1502    DOI: 10.11900/0412.1961.2025.00364
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Microstructural Inheritance Behavior and Mechanical Property Control of TA18 Alloy From Ingot to Tube Blank
LI Shuaiyu1, LIU Zedong1, YANG Jieren1(), JIN Wei2, PENG Bo1, DU Xin1, ZHOU Siman1
1 College of Materials Science and Engineering, Sichuan University, Chengdu 610065, China
2 Shi -changxu Innovation Center for Advanced Materials, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
Cite this article: 

LI Shuaiyu, LIU Zedong, YANG Jieren, JIN Wei, PENG Bo, DU Xin, ZHOU Siman. Microstructural Inheritance Behavior and Mechanical Property Control of TA18 Alloy From Ingot to Tube Blank. Acta Metall Sin, 2026, 62(9): 1487-1502.

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Abstract  

In metallic material processing, the microstructural and textural characteristics developed during each manufacturing stage establish the structural foundation for subsequent processing operations, creating substantial hereditary effects throughout the multistage manufacturing chain. This progressive, cross-process accumulation of microstructural and textural evolution makes precise tracing and effective control of microstructural inheritance pathways particularly complex during full-scale manufacturing from the initial ingot to the final TA18 tube blank. Microstructural inheritance forms the basis for structural design and property optimization in TA18 alloys. This investigation employed a 700-mm diameter TA18 alloy ingot as the starting material. The thermomechanical processing route comprised three stages: initial multipass forging in the β-phase field (1150-950 oC) followed by forging in the α + β phase field at 900 oC to produce a 170-mm diameter rough-forged bar; subsequent processing of the rough-forged bar in the two-phase region at 850 oC to obtain a 125-mm diameter finish-forged bar; finally, peeling, drilling, and canned hot extrusion of the finish-forged bar to fabricate tube blanks with inner and outer diameters of 28 and 42 mm, respectively. This study systematically investigates the hereditary evolution of microstructure and texture throughout the processing route from ingot to tube blank in the TA18 alloy and evaluates its impact on mechanical properties to guide the integrated control of multiscale microstructure and performance. The results demonstrate that microstructural hereditary characteristics can be categorized into three primary types. (1) Once established during rough forging, the micron-scale grain size and equiaxed α-phase morphology remain stably inherited in subsequent processing stages. Grain refinement serves as the fundamental basis for increasing axial tensile strength from 400 MPa to 550 MPa and improving elongation. (2) The inheritance of low angle grain boundary (LAGB) fraction exhibits dynamic evolution. The high fraction inherited during the rough- and finish-forging stages contributes to work hardening but negatively affects plasticity; in contrast, the low fraction inherited after extrusion, achieved via dynamic recrystallization, results in plasticity recovery. (3) The inheritance of crystallographic texture is governed by multiple competing mechanisms. The {0001}//axial direction (AD) basal texture and the <101¯0>//AD texture originating from the central region of the ingot are strongly inherited during subsequent processing, with the intensity of the <101¯0>//AD texture continuously increasing. The c-axis orientation of the α-phase undergoes controlled evolution during processing: it is randomly distributed after rough forging, transforms into a radial texture after finish forging, and finally develops into a circumferential texture after extrusion. The TA18 alloy controls the inheritance and evolution of crystallographic orientation through the competition and synergy of various mechanisms, including initial crystallographic orientation, deformation, and dynamic recrystallization. The integrated design of TA18 alloy tube blanks, possessing high strength and good plasticity can be achieved by reinforcing beneficial hereditary features (such as fine grains and favorable texture) and interrupting harmful features (such as high LAGB fraction and unfavorable texture).

Key words:  TA18 alloy      microstructural inheritance      texture      mechanical property control     
Received:  12 November 2025     
ZTFLH:  TG306  
Fund: National Key Research and Development Program of China(2023YFB3710700)
Corresponding Authors:  YANG Jieren, professor, Tel: 15881010703, E-mail: yangjieren@scu.edu.cn

URL: 

https://www.ams.org.cn/EN/10.11900/0412.1961.2025.00364     OR     https://www.ams.org.cn/EN/Y2026/V62/I9/1487

Fig.1  Schematic of thermomechanical processing route and dimension of tensile sample of TA18 alloy (unit: mm. AD—axial direction, CD—circumferential direction, RD—radial direction)
Fig.2  Microstructures and EDS elemental mappings of TA18 alloy ingots at different locations and after multi-stage hot processing (a, b, b1) OM image (a), low (b) and high (b1) magnified SEM images at edge of the ingot (c, d, d1) OM image (c), low (d) and high (d1) magnified SEM images at D / 4 position of the ingot (D—diameter of the ingot) (e, f, f1) OM image (e), low (f) and high (f1) magnified SEM images at D / 2 position of the ingot (g, g1, h, h1) low (g, h) and high (g1, h1) magnified SEM images of the rough-forged bar in longitudinal section (g, g1) and cross section (h, h1) (DRX—dynamic recrystallization) (i, i1, j, j1) low (i, j) and high (i1, j1) magnified SEM images of the finish-forged bar in longitudinal section (i, i1) and cross section (j, j1) (k, k1) low (k) and high (k1) magnified SEM images of the extruded billet (k2-k4) EDS elemental mappings corresponding to Fig.2k1
PointTiAlV
194.952.952.10
286.711.8911.40
Table 1  EDS point analysis results for points 1 and 2 in Fig.2k1
Fig.3  EBSD orientation maps (a1-f1), pole figures (PFs) (a2-f2), and inverse pole figures (IPFs) (a3-f3) of TA18 alloy ingots at different locations and after multi-stage hot processing (a1-a3) edge of the ingot (b1-b3) D / 4 position of the ingot (c1-c3) D / 2 position of the ingot (d1-d3) rough-forged bar (e1-e3) finish-forged bar (f1-f3) extruded billet
Fig.4  Grain boundary maps (a, c, e, g, i, k), kernel average misorientation (KAM) maps (b, d, f, h, j, l) and corresponding distributions (insets), LAGB/HAGB fractions (m), and misorientation angle distributions (n) of TA18 alloy ingots at different locations and after multi-stage hot processing (LAGB—low angle grain boundary, HAGB—high angle grain boundary. KAM¯—average KAM) (a, b) edge of the ingot (c, d) D / 4 position of the ingot (e, f) D / 2 position of the ingot (g, h) rough-forged bar (i, j) finish-forged bar (k, l) extruded billet
Fig.5  Engineering stress-strain curves (a), mechanical properties (b), and contributions from several strengthening mechanisms to yield strength (c) of TA18 alloy ingots at different locations and after multi-stage hot processing (σρ —contribution of dislocation strengthening to yield strength, σH-P—contribution of fine grain strengthening to yield strength, σ0—matrix strength)
Fig.6  Low (a-f) and high (a1-f1) magnified SEM images of fracture morphologies of TA18 alloy ingot at different locations and after multi-stage hot processing (a, a1) edge of the ingot (b, b1) D / 4 position of the ingot (c, c1) D / 2 position of the ingot (d, d1) rough-forged bar (e, e1) finish-forged bar (f, f1) extruded billet
Fig.7  Schematics of microstructural evolution and inheritance chain
(a) grain fragmentation during hot working (G—original grain, G1—fragmented grain 1, G2—fragmented grain 2)
(b) microstructural inheritance chain during multi-stage thermomechanical processing from ingot to tube blank
Fig.8  EBSD analyses (a-f, a1-a5) and schematics showing the evolution of crystal orientation (g) during thermomechanical processing (a-c) grain orientation spread (GOS) maps corresponding to the rough-forged (a), finish-forged (b), and extruded (c) conditions (a1, a2) enlarged GOS maps of the rectangle regions I (a1) and II (a2) in Fig.8a (G1-G5 represent different grains, and S1-S3 represent different subgrains) (a3) schematic of the crystal structures for subgrains S1-S3 marked in Fig.8a2 (a4, a5) misorientation angle profiles along lines L1 (a4) and L2 (a5) in Fig.8a2, respectively (d-f) PFs and IPFs corresponding to the rough-forged (d), finish-forged (e), and extruded (f) conditions
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