Study on Preparation Process and Interface Microstructure of Titanium–Aluminum Composite Structure
ZHAO Shuo1, JIANG Xintong1, MA Yixin2, MO Lijiang3, REN Yuhang1, YANG Guang2, WANG Xiangming4
1. Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process, Shenyang Aerospace University, Shenyang 110136, China;
2. College of Mechanical and Electrical Engineering, Shenyang Aerospace University, Shenyang 110136, China;
3. Shenyang Rongchuang Precision Manufacturing Co., Shenyang 110168, China;
4. AVIC Shenyang Aircraft Design Research Institute, Shenyang 110035, China
In this paper, the high-strength titanium alloy skeleton structure was prepared by laser selective melting (SLM). Titanium–aluminum composite with different thickness and crystal morphology was formed by smelting the filled aluminum powder/bulk. It was found that diffusion reaction occurred between the interface of Ti–6Al–4V strengthening skeleton and Al–Mg–Sr–Zr alloy matrix, forming a dense metallurgical bonding. The precipitated phases in the interface were mainly TiAl3, TiAl, TiAl2 and Ti3Al5. With the increase of smelting temperature and holding time, thickness of the interface reaction layer gradually increased, reaching 600 μm at 800 ℃–1 h, which proves strong bonding of the composite structure interface. The elastic modulus of the reinforced skeleton, aluminum alloy matrix and reaction interface was analyzed. It was found that the elastic modulus of the reaction layer (1.2×1011 Pa) was higher than that of the titanium alloy reinforced skeleton (1.07×1011 Pa) and the aluminum alloy matrix (7.1×1010 Pa). The results provide theoretical basis for the spatial controllable strengthening of aluminum alloys, which is expected to overcome the inverse relationship between strength and toughness of traditional materials.
赵朔,姜欣彤,马一鑫,莫漓江,任宇航,杨光,王向明. 钛–铝复合结构制备工艺与界面微观组织研究[J]. 航空制造技术, 2024, 67(22): 60-67.
ZHAO Shuo, JIANG Xintong, MA Yixin, MO Lijiang, REN Yuhang, YANG Guang, WANG Xiangming. Study on Preparation Process and Interface Microstructure of Titanium–Aluminum Composite Structure[J]. Aeronautical Manufacturing Technology, 2024, 67(22): 60-67.