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High surface integrity machining of typical aviation difficult-to-machine material blade

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Abstract

The exceptional mechanical properties of titanium alloy and nickel-based high-temperature alloy make them extensively utilized in aero-engine blades. The machinability of these materials is poor due to their high material strength and low thermal conductivity which lead to technical difficulties such as cutting heat accumulation, tool wear, and poor surface quality during the machining process. This study commences with an investigation into the material properties and processing mechanisms of titanium alloy and nickel-based high-temperature alloy, with a particular focus on recent advancements in cutting dynamics, chip formation mechanisms, tool wear, and surface integrity. The important effect of reasonable setting of cutting parameters and machining conditions on the machining integrity is discussed. The future trend for high surface integrity machining of titanium alloy and nickel-based high-temperature alloy blade is finally predicted.

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Funding

This research is supported in part by National Natural Science Foundation of China (52305482).

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Authors and Affiliations

  1. Institute for Aero Engine, Tsinghua University, Beijing, 100084, China

    Dongbo Wu

  2. College of Electrical Engineering, Xinjiang University, Urumqi, 830017, China

    Shibo Liu

  3. Research Institute of Aero-Engine, Beihang University, Beijing, 102206, China

    Hui Wang

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  1. Dongbo Wu
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  3. Hui Wang
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Dongbo Wu: original draft writing, modifications, and frameworks.

Shibo Liu: original draft writing.

Hui Wang: writing, review, and editing.

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Correspondence to Hui Wang.

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Wu, D., Liu, S. & Wang, H. High surface integrity machining of typical aviation difficult-to-machine material blade. Int J Adv Manuf Technol 129, 2861–2873 (2023). https://doi.org/10.1007/s00170-023-12533-4

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