daohang fenxiangbox searchbox qikanlogonew daohangnew searchboxnew navrightzone footerzone paper

Thermal Deformation Behavior of TC4ELI-TC21 Gradient Titanium Alloy Fabricated by Laser Deposition Manufacturing AITranslate

Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China;Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China;Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China;Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China;Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China
AITranslate
Publisher: Editorial Office of Rare Metals and Cemented Carbides
Share Citation Information Add to Favorites Download PDF

    Scan to share on WeChat or Moments

Use WeChat scan.
Share with WeChat friends or Moments

Abstract AITranslate

TC4ELI-TC21 gradient titanium alloy material was fabricated via laser deposition manufacturing(LDM).To investigate the feasibility of simultaneously applying micro-casting and forging during the addi-tive manufacturing process of this gradient material,thermal compression tests were conducted at tempera-tures of 850℃,900℃,950℃and 1000℃and strain rates of 0.01 s-1,0.1 s-1,1 s-1 and 10 s-1.The in-fluence of deformation temperature and strain rate on the peak stress and microstructural evolution beha-vior was analyzed.The results indicate that the TC4ELI-TC21 gradient titanium alloy fabricated by LDM exhibit highly consistent microstructural evolution and integrated mechanical behavior during thermal de-formation.The alloy demonstrates pronounced dynamic softening at elevated temperatures,with peak stress decreasing with increasing temperature and increasing with increasing strain rate.As the deformation temperature increases,the lamellarαphase undergoes dynamic recrystallization,transforming into equiaxedαphase.Furthermore,the volume fraction of equiaxedαphase gradually decreases with increasing strain rate.When the deformation temperature reaches 1000℃,a martensitic transformation occurs within the material,resulting in a microstructure dominated by martensite.Based on the hyperbolic sine-modified Ar-rhenius model,the constitutive equation and thermal processing map were established for the thermal de-formation of LDM-fabricated TC4ELI-TC21 gradient titanium alloy.Based on the instability regions and power dissipation characteristics revealed by the thermal processing map,the optimal thermal deformation process window for this alloy is determined to be a deformation temperature of 900~950℃and a strain rate of 0.01~0.1 s-1.

KeyWords AITranslate

laser deposition manufacturing gradient titanium alloy thermal deformation peak stress mi-crostructure constitutive equation thermal processing map
No data

Basic Information:

DOI:

Chinese Library Classification Number:TG146.23[一般工业技术—材料科学与工程];TG665[金属学及工艺—金属材料]

Citation Information:

TC4ELI-TC21 gradient titanium alloy material was fabricated via laser deposition manufacturing(LDM).To investigate the feasibility of simultaneously applying micro-casting and forging during the addi-tive manufacturing process of this gradient material,thermal compression tests were conducted at tempera-tures of 850℃,900℃,950℃and 1000℃and strain rates of 0.01 s-1,0.1 s-1,1 s-1 and 10 s-1.The in-fluence of deformation temperature and strain rate on the peak stress and microstructural evolution beha-vior was analyzed.The results indicate that the TC4ELI-TC21 gradient titanium alloy fabricated by LDM exhibit highly consistent microstructural evolution and integrated mechanical behavior during thermal de-formation.The alloy demonstrates pronounced dynamic softening at elevated temperatures,with peak stress decreasing with increasing temperature and increasing with increasing strain rate.As the deformation temperature increases,the lamellarαphase undergoes dynamic recrystallization,transforming into equiaxedαphase.Furthermore,the volume fraction of equiaxedαphase gradually decreases with increasing strain rate.When the deformation temperature reaches 1000℃,a martensitic transformation occurs within the material,resulting in a microstructure dominated by martensite.Based on the hyperbolic sine-modified Ar-rhenius model,the constitutive equation and thermal processing map were established for the thermal de-formation of LDM-fabricated TC4ELI-TC21 gradient titanium alloy.Based on the instability regions and power dissipation characteristics revealed by the thermal processing map,the optimal thermal deformation process window for this alloy is determined to be a deformation temperature of 900~950℃and a strain rate of 0.01~0.1 s-1.

quote

GB/T 7714-2015 [1] CUI Can, YANG Xingyuan, ZHANG Rui, et al. Thermal Deformation Behavior of TC4ELI-TC21 Gradient Titanium Alloy Fabricated by Laser Deposition Manufacturing[J]. Rare Metals and Cemented Carbides, 2026(2): 102-111.
MLA [1] CUI Can, et al., "Thermal Deformation Behavior of TC4ELI-TC21 Gradient Titanium Alloy Fabricated by Laser Deposition Manufacturing." Rare Metals and Cemented Carbides, no. 2, 2026, pp. 102-111.
APA [1] CUI Can, YANG Xingyuan, ZHANG Rui, REN Dechun, & JI Haibin. (2026). Thermal Deformation Behavior of TC4ELI-TC21 Gradient Titanium Alloy Fabricated by Laser Deposition Manufacturing. Rare Metals and Cemented Carbides(2), 102-111.
IEEE [1] CUI Can, YANG Xingyuan, ZHANG Rui, REN Dechun, and JI Haibin, "Thermal Deformation Behavior of TC4ELI-TC21 Gradient Titanium Alloy Fabricated by Laser Deposition Manufacturing," Rare Metals and Cemented Carbides, no. 2, pp. 102-111, 2026. keywords: {laser deposition manufacturing;gradient titanium alloy;thermal deformation;peak stress;mi-crostructure;constitutive equation;thermal processing map}