连续SiC纤维增强钛基复合材料应用及研究进展
Application and research progress of continuous SiC fiber reinforced titanium matrix composite materials
查看参考文献73篇
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文摘
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连续SiC纤维增强钛基(SiC_f/Ti)复合材料具有比强度高、比模量高、耐高温等特点,在航空航天领域具有重要的应用前景。本文总结了SiC_f/Ti复合材料的应用、制备、性能调控和检测技术,并提出了SiC_f/Ti复合材料未来需要突破的瓶颈问题。SiC_f/Ti复合材料单向性能优异,在环类转动件(叶环、涡轮盘等)、杆件(涡轮轴、连杆、紧固件等)以及板类构件(飞机蒙皮等)具有明显应用优势。常用的SiC_f/Ti复合材料的制备方法有箔压法和基体涂层法,箔压法适合制备板类结构件,基体涂层法适用于缠绕形式的结构件,如环、盘以及杆等。SiC_f/Ti复合材料的性能主要取决于SiC纤维、钛合金基体以及纤维/基体界面。SiC纤维微观结构和性能对制备工艺具有较强的敏感性,通过反应器结构和沉积条件调控获得性能稳定的SiC纤维是研究重点之一。钛合金基体可通过物理气相沉积的方法涂敷到纤维表面,制备出钛合金先驱丝,这是后续制备出高质量构件的关键。界面微观结构、热稳定性、力学性能与纤维表面的涂层密切相关,因此涂层种类和结构调控是SiC_f/Ti复合材料的界面性能调控的重要手段。 SiC_f/Ti复合材料的应用促进了无损检测技术的发展,由此研究者开展了超声检测、X射线检测和声发射等在复合材料检测上的基础研究。为了实现SiC_f/Ti复合材料的广泛应用,未来还需要在复合材料结构设计、低成本制造、失效分析与寿命预测等方面开展进一步的研究工作。 |
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其他语种文摘
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Continuous SiC fiber reinforced titanium matrix(SiC_f/Ti) composite exhibiting high specific strength, high specific modulus and high temperature resistance, shows important application prospects in the aerospace field. In this paper, the development of SiC_f/Ti composite's application, preparation, property control and testing technology is summarized, and the bottleneck problems required to be broken through are raised. SiC_f/Ti composite shows the unidirectional performance advantages, making it suitable for rotating ring parts(bling, turbine disk, etc), rod parts(turboshaft, connecting rod, fastener, etc) and plate parts(aircraft skin, etc). The commonly used preparation methods of SiC_f/Ti composite materials are foil-fiber-foil(FFF) method and matrix coating technology(MCT). FFF is suitable for preparing plate structural parts,and MCT is suitable for winding structural parts, such as rings, disks and shafts. The properties of SiC_f/Ti composite mainly depend on SiC fiber, titanium alloy matrix and fiber/matrix interface. The microstructure and properties of SiC fibers are highly sensitive to the preparation process,and it is one of the research focuses to obtain stable SiC fibers by regulating the reactor structure and deposition conditions. The titanium alloy matrix can be coated on the fiber surface by physical vapor deposition to prepare the titanium alloy precursor wire,which is the key to the subsequent preparation of high-quality components. The interfacial microstructure,thermal stability and mechanical properties of SiC_f/Ti composites are closely related to the coating on the fiber surface, so the control of coating type and structure is an important means to control the interfacial properties of SiC_f/Ti composites. The application of SiC_f/Ti composite materials has promoted the development of non-destructive testing technology, so researchers have carried out the basic research of ultrasonic testing,X-ray testing and acoustic emission in application of composite material testing. In order to realize the wide application of SiC_f/Ti composites,further research work should be carried out in the structural design,low-cost manufacturing,failure analysis and life prediction of composite materials in the future. |
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来源
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航空材料学报
,2023,43(6):1-19 【核心库】
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DOI
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10.11868/j.issn.1005-5053.2023.000065
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关键词
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SiC_f/Ti复合材料
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应用
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制备技术
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无损检测技术
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地址
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中国航发北京航空材料研究院, 北京, 100095
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中国航空发动机集团先进钛合金重点实验室, 北京, 100095
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语种
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中文 |
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文献类型
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综述型 |
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ISSN
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1005-5053 |
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学科
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一般工业技术 |
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文献收藏号
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CSCD:7642443
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