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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2021, Vol. 42 ›› Issue (10): 525430-525430.doi: 10.7527/S1000-6893.2021.25430

• Article • Previous Articles    

Laser additive manufactured high strength-toughness TC11 titanium alloy: Mechanical properties and application in airframe load-bearing structure

ZHANG Jikui1,2, KONG Xiangyi3, MA Shaojun4, LIU Dong1,5, WANG Xinbo6, FENG Jun6, WANG Huaming1,2   

  1. 1. National Engineering Laboratory of Additive Manufacturing for Large Metallic Components, Beihang University, Beijing 100083, China;
    2. Research Institute of Frontier Science, Beihang University, Beijing 100083, China;
    3. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China;
    4. AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
    5. Beijing Yuding Advanced Materials & Manufacturing Technologies Co, Ltd., Beijing 100096, China;
    6. AVIC the First Aircraft Institute, Xi'an 710089, China
  • Received:2021-03-01 Revised:2021-03-19 Published:2021-04-29
  • Supported by:
    National Natural Science Foundation of China (51775018); Aeronautical Science Foundation of China (2016ZA51008)

Abstract: With the development of damage tolerance design concept and increasing requirement for lightweight, the high strength-toughness titanium alloy has been the main airframe material of load-bearing structure. Laser additive manufacturing has the advantages of digitization, short period and low cost in deposition of the large load bearing structure. Especially, the dynamics of solid phase transformation in the laser additive manufacturing process provide a new opportunity for the preparation of high strength-toughness titanium alloy. In this paper, the static strength, fatigue and damage tolerant properties of the laser additive manufactured TC11 titanium alloy were reported and analyzed according to the design requirements of airframe load-bearing structure. The prospects of using the alloy for the airframe load-bearing structure are then discussed. The results show that the alloy is characterized by high strength-toughness and low yield strength ratio. With low fatigue notch sensitivity, low fatigue crack growth rate and small dispersibility, the alloy can meet the requirements of mechanical properties of the airframe load-bearing structure. Compared with the damage tolerant TC4-DT titanium alloy that is now widely used for the airframe load-bearing structure, the laser additive manufactured TC11 titanium alloy shows similar damage tolerant properties, better fatigue performance, and improved static strength (by 23%). The excellent strength/toughness matching of the laser additive manufactured TC11 titanium alloy can avoid the occurrence of low stress brittle fracture in large thickness components, and low fatigue notch sensitivity and fatigue crack growth rate of the alloy are critical for ensuring service safety of the airframe load-bearing structure.

Key words: laser additive manufacture, titanium alloy, load-bearing structure, static strength, fatigue, damage tolerance

CLC Number: