Status and role of the advanced composite materials in the development of aviation equipment
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摘要: “一代材料,一代装备”阐明了材料技术在装备发展中的重要性。航空装备的发展历程表明,一代新材料的出现支撑了一代新装备的研发,一代新装备的研制牵引一代新材料的应用。不同航空装备应用不同的结构材料,和三代机相比,四代战斗机用结构材料的最大差别是先进复合材料的大量应用。本文介绍了国内先进复合材料技术的发展历程和现状、复合材料技术发展面临的机遇和挑战及今后国内先进复合材料技术的发展重点。Abstract: "One generation of new materials, one generation of new equipment" illustrates the importance of material technology in the development of equipment. The development history of aviation equipment shows that the research and development of a new equipment is always supported by a new generation of materials, and the development of a new generation of equipment leads the application of a new generation of materials. That is to say the different aviation equipment uses different structural materials. The fourth-generation aircraft had a very marked difference with the third-generation aircraft on the usage of structural materials. The advanced composites are widely used for structural materials in the fourth-generation aircraft. In this article, the development process and current situation of domestic aviation composite technology is reviewed. The opportunities and challenges of the advanced composite technology are introduced. The significant future trends of domestic advanced composite technology are also proposed.
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表 1 先进复合材料的主要应用
Table 1. Main applications of composites in aviation
Composites Applications Carbon fiber structure materials Mainly used for load-bearing components to reduce the structure weight of the aircraft Structure wave- absorbing integration composites Mainly used for strong radar scattering source stealth components of aircraft to achieve the desired radar cross-sectional (RCS) reduction effect Structure wave-transmitting integration composites Mainly used for detection/communication windows to support the detection and electronic warfare capabilities of the aircraft 表 2 国内部分聚酰亚胺(PI)纤维的基本性能
Table 2. Properties of several domestic polyimide (PI) fiber
PI fiber Tensile strength/GPa Tensile modulus/GPa Tg/℃ S30 3.0±0.2 110±5 ≥330 S30 M 3.0±0.2 140±5 ≥340 S35 M 3.5±0.2 150±5 ≥340 S40 4.0±0.2 140±5 ≥340 Note: Tg—Glass transition temperature. 表 3 部分结构透波复合材料的介电性能
Table 3. Dielectric properties of several structure wave-transmitting composites
Properties Glass/
EpoxyQuartz/
EpoxyQuartz/
CyanateQuartz/
BMIService temperature/℃ 80 100 170 150 Dielectric constant 4.23 3.38 3.53 3.58 Loss tangent 0.018 0.010 0.006 0.0079 -
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