2AlNb;氣壓脹形;熱成形性;微觀組織"/>

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Ti-22Al-25Nb合金板材氣壓脹形實驗及數(shù)值模擬
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作者單位:

1.太原理工大學 材料科學與工程學院,山西 太原 030024;2.哈爾濱工業(yè)大學 金屬精密熱加工國家級重點實驗室,黑龍江 哈爾濱 150001

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基金項目:

國家自然科學基金青年科學基金項目(51505323),山西省應用基礎研究計劃項目(20210302123117, 20210302124658)


Experiment and Numerical Simulation of Ti-22Al-25Nb Alloy Sheet by Gas Bulging
Author:
Affiliation:

1.College of Materials Science and Engineering, Taiyuan University of Technology, Taiyuan 030024, China;2.National Key Laboratory of Science and Technology on Precision Heat Processing of Metals, Harbin Institute of Technology, Harbin 150001, China

Fund Project:

National Natural Science Foundation of China (51505323); Applied Basic Research Program of Shanxi Province (20210302123117, 20210302124658)

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    摘要:

    通過氣壓脹形實驗和數(shù)值模擬研究了Ti-22Al-25Nb合金板材在高溫下的熱成形行為,并分析了在930和970 ℃下的脹形球殼形狀和壁厚分布,討論了脹形部分的微觀結構和力學性能。結果表明,在脹形初期,脹形球殼接近球面,隨脹形高度的增加逐漸橢球化。在930和970 ℃下,最終脹形高度分別達到46.25和49.85 mm,殼頂?shù)那拾霃椒謩e達到49.33和49.19 mm。脹形部分壁厚不均勻,從底部至頂部逐漸減小。變形溫度對球殼形狀影響較大,在930 ℃時脹形局部形狀更加不均。在相同的脹形高度下,930 ℃下的脹形球殼曲率半徑較小且壁厚減薄率較高。此外,在930 ℃脹形過程中,O相析出并球化,導致O型、V型空洞的產生且硬度下降。而在970 ℃脹形后,微觀組織分布均勻,O相在冷卻過程中以層片形式析出,強化了脹形件。

    Abstract:

    The hot formability of Ti-22Al-25Nb alloy sheet at elevated temperatures was studied through the gas bulging experiments and numerical simulation. The distributions of bulging shell shape and wall thickness at 930 and 970 °C were analyzed. The microstructure and mechanical properties of the bulging part were discussed. Results show that the bulging shell is close to the spherical surface in the initial bulging stage, and it gradually becomes ellipsoid with increasing the bulging height. At 930 and 970 °C, the final bulging height reaches 46.25 and 49.85 mm, and the curvature radius of shell top reaches 49.33 and 49.19 mm, respectively. The wall thickness of bulging part is inhomogeneous: it gradually decreases from the bottom region to the top region. The deformation temperature strongly affects the shape of bulging part: the partial bulging shape is more inhomogeneous at low temperature of 930 °C. Under the same bulging height, the curvature radius of bulging is lower and the thinning ratio is higher at 930 °C. In addition, the O phase is precipitated and spheroidized during bulging at 930 °C, which causes the generation of O type and V type cavities and the reduction in microhardness. However, the microstructure is uniformly distributed after bulging at 970 °C. O phase is precipitated during the cooling process in lamellar morphology, which strengthens the bulging part.

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殷宏亮,孟令健,魯羽鵬,林鵬.Ti-22Al-25Nb合金板材氣壓脹形實驗及數(shù)值模擬[J].稀有金屬材料與工程,2023,52(3):806~814.[Yin Hongliang, Meng Lingjian, Lu Yupeng, Lin Peng. Experiment and Numerical Simulation of Ti-22Al-25Nb Alloy Sheet by Gas Bulging[J]. Rare Metal Materials and Engineering,2023,52(3):806~814.]
DOI:10.12442/j. issn.1002-185X.20220644

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歷史
  • 收稿日期:2022-08-08
  • 最后修改日期:2022-09-05
  • 錄用日期:2022-09-27
  • 在線發(fā)布日期: 2023-03-31
  • 出版日期: 2023-03-24