Fu Xinpeng, Li Boya, Fu Binguo, Dong Tianshun, Li Jingkun
State Key Laboratory of High Performance Roll Materials and Composite Forming, School of Materials Science and Engineering, Hebei University of Technology, Tianjin 300401, China.
Hebei Key Laboratory of New Functional Materials, School of Materials Science and Engineering, Hebei University of Technology, Tianjin 300401, China.
Materials (Basel). 2025 Jun 30;18(13):3099. doi: 10.3390/ma18133099.
The application fields of high-temperature titanium alloys are mainly concentrated in the aerospace, defense and military industries, such as the high-temperature parts of rocket and aircraft engines, missile cases, tail rudders, etc., which can greatly reduce the weight of aircraft while resisting high temperatures. However, traditional high-temperature titanium alloys containing multiple types of elements (more than six) have a complex impact on the solidification, deformation, and phase transformation processes of the alloys, which greatly increases the difficulty of casting and deformation manufacturing of aerospace and military components. Therefore, developing low-component high-temperature titanium alloys suitable for hot processing and forming is urgent. This study used data augmentation (Gaussian noise) to expedite the development of a novel quinary high-temperature titanium alloy. Utilizing data augmentation, the generalization abilities of four machine learning models (XGBoost, RF, AdaBoost, Lasso) were effectively improved, with the XGBoost model demonstrating superior prediction accuracy (with an R value of 0.94, an RMSE of 53.31, and an MAE of 42.93 in the test set). Based on this model, a novel Ti-7.2Al-1.8Mo-2.0Nb-0.4Si (wt.%) alloy was designed and experimentally validated. The UTS of the alloy at 600 °C was 629 MPa, closely aligning with the value (649 MPa) predicted by the model, with an error of 3.2%. Compared to as-cast Ti1100 and Ti6242S alloy (both containing six elements), the novel quinary alloy has considerable high-temperature (600 °C) mechanical properties and fewer components. The microstructure analysis revealed that the designed alloy was an α+β type alloy, featuring a typical Widmanstätten structure. The fracture form of the alloy was a mixture of brittle and ductile fracture at both room and high temperatures.
高温钛合金的应用领域主要集中在航空航天、国防军工等行业,如火箭和飞机发动机的高温部件、导弹壳体、尾舵等,在耐高温的同时可大幅减轻飞行器重量。然而,传统的含多种元素(六种以上)的高温钛合金对合金的凝固、变形及相变过程有复杂影响,极大增加了航空航天及军工零部件的铸造和变形制造难度。因此,开发适用于热加工和成型的低组元高温钛合金迫在眉睫。本研究采用数据增强(高斯噪声)来加速新型五元高温钛合金的开发。通过数据增强,有效提高了四种机器学习模型(XGBoost、RF、AdaBoost、Lasso)的泛化能力,其中XGBoost模型在测试集中表现出卓越的预测精度(R值为0.94,RMSE为53.31,MAE为42.93)。基于该模型,设计并通过实验验证了一种新型Ti-7.2Al-1.8Mo-2.0Nb-0.4Si(wt.%)合金。该合金在600℃时的抗拉强度为629MPa,与模型预测值(649MPa)紧密吻合,误差为3.2%。与铸态Ti1100和Ti6242S合金(均含六种元素)相比,这种新型五元合金具有相当可观的高温(600℃)力学性能且组元更少。微观结构分析表明,所设计的合金为α+β型合金,具有典型的魏氏组织。该合金在室温和高温下的断裂形式均为脆性和韧性断裂的混合。