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Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (13): 629471-629471.doi: 10.7527/S1000-6893.2023.29471

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Material removal mechanism and surface integrity of cutting titanium aluminum alloy under different cooling conditions

Xiangyu WANG, Jinhui WANG, Wenhao QIU, Jintao NIU, Xiuli FU, Yang QIAO()   

  1. School of Mechanical Engineering,University of Jinan,Jinan 250022,China
  • Received:2023-08-23 Revised:2023-09-21 Accepted:2023-10-04 Online:2024-07-15 Published:2023-12-21
  • Contact: Yang QIAO E-mail:me_qiaoy@ujn.edu.cn
  • Supported by:
    National Natural Science Foundation of China(52005215);Shandong Province Higher Education Science and Technology Plan(2019KJB021)

Abstract:

Titanium aluminum alloy has such advantages as low density, high strength, good high-temperature creep resistance and oxidation resistance, and has broad application prospects in the aerospace industry. However, due to the poor thermal conductivity, severe work hardening, and low-temperature brittleness of the material, the high cutting temperature during the cutting processing leads to low machining efficiency, low tool life, and poor surface integrity, which limits the application promotion of this material. this paper Focusing on the problem of high cutting temperature of titanium aluminum alloy, and based on its temperature sensitive mechanical properties, this paper investigates the mechanical properties, material removal mechanism, and surface integrity of titanium aluminum alloy Ti-48Al-2Cr-2Nb material. The dynamic failure behavior and fracture mechanism of the material at different temperatures are studied through Hopkinson impact shear tests. The chip morphology and morphology evolution under different cooling conditions and cutting parameters are simulated through finite element simulation. Face turning experiments are conducted under three different cooling environments, and the changing rule of surface roughness is analyzed. Combining the fracture mechanism of the material and the fracture form of the lamellar structure, the formation mechanisms of micro pits and microcracks are revealed. The degree of work hardening and the depth of the hardened layer are analyzed by combining cutting force and cutting temperature, revealing the changing rule of hardness.

Key words: cooling conditions, cutting temperature, titanium aluminum alloy, surface integrity, material removal mechanism

CLC Number: