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Effect of initial residual stress on mechanical properties of ZTC4 titanium alloy
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Jun LUO1, 2, 3, Xi WANG1, 2, 3, Wenzheng ZHAO1, 4, Hai NAN1, 4, Changkui LIU1, 2, 3, Nan LI1, 2, 3
Journal of Materials Engineering | 2026, 54(4) : 269 - 281
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Journal of Materials Engineering | 2026, 54(4): 269-281
• RESEARCH ARTICLE •
Effect of initial residual stress on mechanical properties of ZTC4 titanium alloy
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Jun LUO1, 2, 3, Xi WANG1, 2, 3, Wenzheng ZHAO1, 4, Hai NAN1, 4, Changkui LIU1, 2, 3, Nan LI1, 2, 3
Affiliations
  • 1.AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
  • 2.Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation,Beijing 100095,China
  • 3.Key Laboratory of Aeronautical Materials Testing and Evaluation,Aero Engine Corporation of China,Beijing 100095,China
  • 4.Beijing Engineering Research Center of Advanced Titanium Alloy Precision Forming Technology,Beijing 100095,China
Published: 2026-04-20 doi: 10.11868/j.issn.1001-4381.2024.000604
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The microstructure, tensile fracture morphology and initial residual stress of ZTC4 titanium alloy repair welding are analyzed by stereomicroscope, optical microscope (OM), scanning electron microscope (SEM), X-ray residual stress analyzer and tensile testing machine, and their effects on room temperature/high temperature tensile properties and fatigue properties are studied. The results show that the microstructure of ZTC4 titanium alloy after repair welding is mainly composed of equiaxed grains (with a grain size of about 1.5 mm) and grains with a large aspect ratio (5∶1). Different repair welding diameters and annealing treatment can affect the properties of residual stress, thus affecting the mechanical properties. The residual stress at the center of the original state of the room temperature/high temperature tensile and fatigue specimens is mainly tensile stress, which is 115.9, -24.6 MPa and 55.6 MPa, respectively. In the high temperature (350 ℃) tensile test, the larger the initial residual tensile stress (173.3 MPa) at the center of the repair welding diameter 4 mm specimens, the lower the tensile strength (710.7 MPa); the larger the initial residual compressive stress (-159.1 MPa) at the center of the repair welding diameter 4 mm and annealing specimens, the higher the tensile strength (749.3 MPa).The residual tensile stress significantly shortens the fatigue life of titanium alloy, whereas residual compressive stress increases it. The initial residual stress at the center of the original state, repair welding diameter of 2 mm, repair welding diameter of 2 mm and annealing, repair welding diameter of 4 mm, and repair welding diameter of 4 mm and annealing specimen is 55.6,109.9, -189.1,61.4 MPa, and -64.3 MPa, respectively. The fatigue properties of the specimens with initial residual compressive stress is better.

ZTC4 titanium alloy  /  residual stress  /  tensile property  /  fatigue property
罗军, 王曦, 赵文正, 南海, 刘昌奎, 李楠. 初始残余应力对ZTC4钛合金力学性能的影响. 材料工程, 2026 , 54 (4) : 269 -281 . DOI: 10.11868/j.issn.1001-4381.2024.000604
Jun LUO, Xi WANG, Wenzheng ZHAO, Hai NAN, Changkui LIU, Nan LI. Effect of initial residual stress on mechanical properties of ZTC4 titanium alloy[J]. Journal of Materials Engineering, 2026 , 54 (4) : 269 -281 . DOI: 10.11868/j.issn.1001-4381.2024.000604
Year 2026 volume 54 Issue 4
72
33
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Article Info
doi: 10.11868/j.issn.1001-4381.2024.000604
  • Receive Date:2024-08-27
  • Online Date:2026-10-27
  • Published:2026-04-20
Article Data
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History
  • Received:2024-08-27
  • Accepted:2024-12-03
Funding
Affiliations
    1.AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
    2.Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation,Beijing 100095,China
    3.Key Laboratory of Aeronautical Materials Testing and Evaluation,Aero Engine Corporation of China,Beijing 100095,China
    4.Beijing Engineering Research Center of Advanced Titanium Alloy Precision Forming Technology,Beijing 100095,China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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