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Research paper | Publishing Language: Chinese | Open Access

Numerical simulation and process optimization of precision casting for large complex thin-walled TiAl alloy compressor casing

Hong HUANG1( )Feng LI2Haitao HU2Xin FENG2Xianfei DING2Hai NAN2Haipeng JIN1Lei YE1
Center of Technology Management & Standardization,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
Cast Titanium Alloy Research and Development Center,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
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Abstract

Based on ProCAST numerical simulation software, the effects of centrifugal casting and gravity casting on the forming of Ti-48Al-2Nb-2Cr alloy diffuser casing are analysed comparatively. The results show that centrifugal pouring at rotational speed of 400 r/min enhances the directional mold filling of molten metal and forced convection during solidification. Compared with gravity pouring, it greatly shortens solidification time and reduces shrinkage porosity volume by 21.8%. A curved riser gating system is innovatively designed to address hot spots in thick-wall regions, transferring defects on the inner ring flange to the risers. This design cuts shrinkage porosity volume by 47.1% relative to the straight risers. Experimental verification confirms that castings fabricated with optimized processes have no internal defects detected by X-ray inspection and no shrinkage porosity observed under microstructure examination. Fine-grained structures with lamellar colonies of 400 μm form in thin-wall support plates due to rapid cooling. Its tensile strength at room temperature and 750 ℃ rises by 4.9% and 10%, respectively, comparing with thick-wall flanges. These findings provide a reliable process scheme for high-quality forming of large-scale complex thin-wall TiAl components.

CLC number: TG146.2;V252.2 Document code: A

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Journal of Aeronautical Materials
Pages 92-101

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Cite this article:
HUANG H, LI F, HU H, et al. Numerical simulation and process optimization of precision casting for large complex thin-walled TiAl alloy compressor casing. Journal of Aeronautical Materials, 2026, 46(7): 92-101. https://doi.org/10.11868/j.issn.1005-5053.2025.000177

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Received: 23 September 2025
Published: 15 July 2026
© Journal of Aeronautical Materials 2026.

This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).