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发动机用耐高温聚酰亚胺树脂基复合材料的研究进展 被引量:60

Advance in High Temperature Polyimide Resin Matrix Composites for Aeroengine
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摘要 综述耐高温热固性聚酰亚胺树脂及复合材料的研究进展。经过近四十年的发展,形成了多种封端剂封端的热固性聚酰亚胺树脂,其中主要是降冰片烯和4-苯乙炔基苯酐封端聚酰亚胺,长期使用温度涵盖280~450℃的聚酰亚胺树脂及其复合材料体系。低成本、高韧性和有机无机杂化聚酰亚胺树脂基复合材料将是聚酰亚胺复合材料发展的主要方向。 Advance in thermosetting polyimide and its composites were reviewed. In the last forty years, many kinds of endcap reagent were fund to synthesis polyimide resin matrix for composites, and most of polyimide was endcaped by Nadic anhydride or PEPA an- hydride. Many series of polyimide resin were developed to the service in 280-450℃ for aeroengine. Low-cost polyimide, high tough- ness polyimide and organic/inorganic hybrid polyimide will be the main directions of polyimide study in the future.
出处 《航空材料学报》 EI CAS CSCD 北大核心 2012年第6期1-13,共13页 Journal of Aeronautical Materials
关键词 发动机 热固性聚酰亚胺 碳纤维 复合材料 aeroengine thermosetting polyimide carbon fiber composites
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