Dispersion, solid solution, and covalent bond coupled to strengthen K4169/TiAl composite brazed joints: first-principles and experimental perspective

IF 11.2 1区 材料科学 Q1 MATERIALS SCIENCE, MULTIDISCIPLINARY Journal of Materials Science & Technology Pub Date : 2024-09-17 DOI:10.1016/j.jmst.2024.08.050
Liangliang Zhang, Peng Li, Honggang Dong
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Abstract

Ni/TiAl composite brazed joints could significantly reduce the aircraft's weight. However, low interfacial adhesion, coarse and brittle-hard intermetallic compounds (IMCs) seriously limited the application of Ni/TiAl composite joints in the next generation of aerospace applications. So enhanced K4169/TiAl composite joints were investigated by vacuum brazed with (Ni53.33Cr20B16.67Si10/Zr25Ti18.75Ta12.5Ni25Cu18.75) composite filler metal (CFM) designed based on cluster-plus-glue-atom model. The shear strength of the joint reached 485 MPa, comparable to the 491 MPa of TiAl substrate. The flat and brittle-hard diffusion reaction layer between Zones I and II was eliminated, simultaneously generating CrB4 dispersion strengthening due to the CFM developed with the interfacial solid-liquid space-time hysteresis effect. In Zones II and III, IMCs all transformed into Niss(Cr,Fe)[0-88], Niss(Ti, Al)[004], and Niss(Zr,Si)[11-2] of circular and oval shapes through isothermal solidification. Meanwhile, the residual stresses and hardness were distributed in reticulated cladding characteristics. Thereby, lattice distortion led to solid solution strengthening and increased plastic toughness through crack termination and bridging mechanisms, which inhibited dislocations from plugging and crack propagation. Various interfaces in Zone Ⅳ were regulated into semi- and coherent interfaces. Ni3(Ti,Al)/(Ni,Ti,Al) and (Ni,Ti,Al)/AlNi2Ti were composed of higher interfacial bonding energy (2.771 J/m2, 2.547 J/m2) and Ni-Ni covalent bonds. Interfacial covalent bonding and large interfacial bonding energy coupling strengthened Zone IV. Consequently, cracks initiated at the (Ni,Ti,Al)[013]/Ti3Al[010] and expanded rapidly into TiAl substrate. Therefore, applying this method to design CFMs and regulate the phase, grain morphology, and interface's fine structure could provide new pathways for dissimilar hard-to-join metals.

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分散、固溶和共价键耦合强化 K4169/TiAl 复合材料钎焊接头:第一原理和实验视角
镍/钛铝复合材料钎焊接头可显著减轻飞机重量。然而,低界面附着力、粗糙且脆硬的金属间化合物(IMC)严重限制了 Ni/TiAl 复合材料接头在下一代航空航天领域的应用。因此,通过真空钎焊与基于簇加胶原子模型设计的(Ni53.33Cr20B16.67Si10/Zr25Ti18.75Ta12.5Ni25Cu18.75)复合填充金属(CFM),研究了增强型 K4169/TiAl 复合材料接头。接头的剪切强度达到 485 兆帕,与钛铝基体的 491 兆帕相当。在 I 区和 II 区之间消除了扁平和脆硬的扩散反应层,同时由于利用界面固液时滞效应开发的 CFM 而产生了 CrB4 分散强化。在 II 区和 III 区,IMC 通过等温凝固全部转化为圆形和椭圆形的 Niss(Cr,Fe)[0-88]、Niss(Ti,Al)[004]和 Niss(Zr,Si)[11-2]。同时,残余应力和硬度分布在网状包层特征中。因此,晶格畸变导致固溶强化,并通过裂纹终止和桥接机制提高塑性韧性,从而抑制位错堵塞和裂纹扩展。Ⅳ区的各种界面被调节为半相干和相干界面。Ni3(Ti,Al)/(Ni,Ti,Al)和(Ni,Ti,Al)/AlNi2Ti由较高的界面键能(2.771 J/m2,2.547 J/m2)和 Ni-Ni 共价键组成。界面共价键和较大的界面键能耦合强化了 IV 区。因此,裂纹从(Ni,Ti,Al)[013]/Ti3Al[010]处开始,并迅速扩展到 TiAl 基底。因此,应用这种方法设计 CFM 并调节相、晶粒形态和界面的精细结构,可为异种难接合金属提供新的途径。
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来源期刊
Journal of Materials Science & Technology
Journal of Materials Science & Technology 工程技术-材料科学:综合
CiteScore
20.00
自引率
11.00%
发文量
995
审稿时长
13 days
期刊介绍: Journal of Materials Science & Technology strives to promote global collaboration in the field of materials science and technology. It primarily publishes original research papers, invited review articles, letters, research notes, and summaries of scientific achievements. The journal covers a wide range of materials science and technology topics, including metallic materials, inorganic nonmetallic materials, and composite materials.
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