国内航空发动机用树脂基复合材料及应用现状

倪洪江 ,  雷帅 ,  王成博 ,  燕吉强 ,  陈祥宝

航空材料学报 ›› 2026, Vol. 46 ›› Issue (5-6) : 7 -23.

PDF (3177KB)
航空材料学报 ›› 2026, Vol. 46 ›› Issue (5-6) : 7 -23. DOI: 10.11868/j.issn.1005-5053.2026.000009

国内航空发动机用树脂基复合材料及应用现状

作者信息 +

Domestic current status of polymer-matrix composite for aero-engines and application

Author information +
文章历史 +
PDF (3253K)

摘要

先进航空发动机性能的提升对整机结构轻量化提出更高要求,树脂基复合材料是实现航空发动机轻量化的关键材料之一。近年来,北京航空材料研究院聚焦航空发动机冷端部件应用的需求,系统研发了航空发动机高韧性环氧树脂、耐高温高韧性双马树脂、耐高温聚酰亚胺树脂以及高韧性热塑性树脂基复合材料。本文在总结国外航空发动机用树脂基复合材料进展概况、航空发动机发展对树脂基复合材料的要求的基础上,以北京航空材料研究院相关研制进展为代表,介绍国内航空发动机用树脂基复合材料研发和应用方面的主要进展,并提出航空发动机用树脂基复合材料未来发展趋势和重点。总体来讲,国内航空发动机用树脂基复合材料在耐高温性能、抗冲击性能、结构功能一体化、整体制造技术等方面取得突破,并实现在航空发动机风扇叶片、包容机匣、外涵机匣等的批量应用。面向未来航空发动机需求,树脂基复合材料将向耐高温化、高韧化、结构整体化、工艺自动化与智能化、全寿命周期低成本化等方向不断聚焦。

Abstract

Performance enhancement of advanced aero-engines sets a higher requirement for their overall structural lightweighting. Polymer-matrix composite (PMC) are one of the key materials to achieve aeroengine lightweighting. In recent years,focusing on the aero-engine cold-section parts, AECC Beijing Institute of Aeronautical Materials (BIAM) has systematically developed PMCs of high-toughness epoxy, high-temperature and high-toughness bismaleimide, high-temperature polyimide and high-toughness thermoplastic resins. This article introduces the foreign profile of PMCs for aero-engines and the demands of aeroengines for PMCs. Then, taking BIAM as the representative, domestic current status of PMCs for aero-engines and application are introduced. PMC development trend and emphasis for aero-engines are proposed. Overall,domestic PMC for aero-engines have made breakthrough in such aspects as high-temperature resistance,impact resistance,structure/function integration and integral fabrication technology,and have achieved batch application in such parts as fan blades, containment casings and outer ducts. For the needs of future aero-engines, PMC would focus more and more on the directions including thermal resistance enhancement, toughness improvement, structure integration,processing automation and intelligentization,full-life cost minimization.

关键词

航空发动机 / 结构轻量化 / 树脂基复合材料 / 热固性树脂 / 热塑性树脂

Key words

aero-engine / structural lightweighting / polymer-matrix composite (PMC) / thermosetting resin / thermoplastic resin

引用本文

引用格式 ▾
倪洪江,雷帅,王成博,燕吉强,陈祥宝. 国内航空发动机用树脂基复合材料及应用现状[J]. 航空材料学报, 2026, 46(5-6): 7-23 DOI:10.11868/j.issn.1005-5053.2026.000009

登录浏览全文

4963

注册一个新账户 忘记密码

参考文献

[1]

陈祥宝. 聚合物基复合材料手册[M]. 北京: 化学工业出版社, 2004.

[2]

CHEN X B. Handbook of polymer matrix compo-sites[M]. Beijing: Chemical Industry Press, 2004.

[3]

沈尔明, 王志宏, 滕佰秋, . 连续纤维增强复合材料在民用航空发动机上的应用[J]. 航空发动机, 2013, 39(2):90-94.

[4]

SHEN E M, WANG Z H, TENG B Q, et al. Application of continuous fiber reinforced composites in civil aero-engines[J]. Aeroengine, 2013, 39(2):90-94.

[5]

赵淼, 张代军. 航空发动机用树脂基复合材料发展现状与应用[J]. 工程塑料应用, 2025, 53(7):198-203.

[6]

ZHAO M, ZHANG D J. Current status and applications of resin matrix composites for aero-engine[J]. Engineer-ing Plastics Application, 2025, 53(7):198-203.

[7]

李军, 刘燕峰, 倪洪江, . 航空发动机用树脂基复合材料应用进展与发展趋势[J]. 材料工程, 2022, 50(6): 49-60.

[8]

LI J, LIU Y F, NI H J, et al. Application progress and development trend of resin matrix composites for aero engine[J]. Journal of Materials Engineering, 2022, 50(6):49-60.

[9]

包建文, 陈祥宝. 发动机用耐高温聚酰亚胺树脂基复合材料的研究进展[J]. 航空材料学报, 2012, 32(6):1-13.

[10]

BAO J W, CHEN X B. Advance in high temperature polyimide resin matrix composites for aeroengine[J]. Journal of Aeronautical Materials, 2012, 32(6):1-13.

[11]

WILSON D. Polyimides as resin matrices for advanced composites[M]. Dordrecht: Springer Netherlands, 1990: 187-226.

[12]

SERAFINI T. Polymer matrix composites research at NASA Lewis Research Center[C]// Advanced Materials Technology Seminar. Hampton, VA, US: National Aero-nautics and Space Administration, 1982.

[13]

包建文, 蒋诗才, 张代军. 航空碳纤维树脂基复合材料的发展现状和趋势[J]. 科技导报, 2018, 36(19):52-63.

[14]

BAO J W, JIANG S C, ZHANG D J. Current status and trends of aeronautical resin matrix composites reinforced by carbon fiber[J]. Science & Technology Review, 2018, 36(19):52-63.

[15]

陈祥宝, 张宝艳, 邢丽英. 先进树脂基复合材料技术发展及应用现状[J]. 中国材料进展, 2009, 28(6):2-12.

[16]

CHEN X B, ZHANG B Y, XING L Y. Application and development of advanced polymer matrix composites[J]. Materials China, 2009, 28(6):2-12.

[17]

王燚林, 刘天生, 刘东, . 航空发动机复合材料静子叶片研究进展[J]. 玻璃钢/复合材料, 2018(12):96-101.

[18]

WANG Y L, LIU T S, LIU D, et al. Research progress of aeroengine composite stator blades[J]. Fiber Reinforced Plastics/Composites, 2018(12):96-101.

[19]

刘强, 赵龙, 黄峰, . 机织复合材料风扇叶片成型技术研究[J]. 纤维复合材料, 2019, 36(4):68-72.

[20]

LIU Q, ZHAO L, HUANG F, et al. Molding process of woven composite fan blades[J]. Fiber Composites, 2019, 36(4):68-72.

[21]

DOREY G, PEEL C J, CURTIS P T. Advanced materi-als for aerospace structures[J]. Journal of Aerospace Engineering, 1994, 208(1):1-8.

[22]

KRISHNAMACHARI P, LOU J Z, SANKAR J, et al. Characterization of fourth-generation high-temperature discontinuous fiber molding compounds[J]. Interna-tional Journal of Polymer Analysis and Characterization, 2009, 14(7):588-599.

[23]

SCOLA D A. Polyimide resins[M]. Ohio: ASM Interna-tional,2001:105-119.

[24]

STENZENBERGER H D. Addition polyimides:high per-formance polymers[M]. Berlin, Heidelberg: Springer Berlin Heidelberg,1994:165-220.

[25]

SERAFINI T T, HANSON P M. Environmental effects on graphite fiber reinforced PMR-15 polyimide: NASA TM[R]. 1980.

[26]

BOWLES K J, JAYNE D, LEONHARDT T A. Thermal stability relationships between PMR-15 resin and its com-posites:NASA 106285[R]. 1993.

[27]

CHUANG K C, BOWLES K J. A high Tg PMR poly-imide composites (DMBZ-15):NASA RTOP 523-31-13[R]. 2000.

[28]

HUTAPEA P, YUAN F G. The effect of thermal aging on the Mode-Ⅰ interlaminar fracture behavior of a high-temperature IM7/LaRC-RP46 composite[J]. Composites Science and Technology, 1999, 59(8):1271-1286.

[29]

LIU Y M, XIAO Y, SUN X, et al. Microwave irradiation of nadic-end-capped polyimide resin (RP-46) and glass-graphite-RP-46 composites: cure and process studies[J]. Journal of Applied Polymer Science, 1999, 73(12) :2391-2411.

[30]

PATER R H, CURTO P A. Advanced materials for space applications[J]. Acta Astronautica, 2007, 61(11/12) : 1121-1129.

[31]

GAO S Q, CH WANG X, HU A J, et al. Preparation and properties of PMR-Ⅱ polyimide/chopped quartz fibre composites[J]. High Performance Polymers, 2000, 12(3):405-417.

[32]

FANG X M, SCOLA D A. Investigation of microwave energy to cure carbon fiber reinforced phenylethynyl-ter-minated polyimide composites, PETI-5/IM7[J]. Journal of Polymer Science Part A, 1999, 37(24):4616-4628.

[33]

CANO R J, JENSEN B J. Effect of molecular weight on processing and adhesive properties of the phenylethynyl-terminated polyimide LARC™-PETI-5[J]. The Journal of Adhesion, 1997, 60(1/4):113-123.

[34]

CONNELL J W, SMITH J G Jr, HERGENROTHER P M, et al. High temperature transfer molding resins:lami-nate properties of PETI-298 and PETI-330[J]. High Per-formance Polymers, 2003, 15(4):375-394.

[35]

YOKOTA R, YAMAMOTO S, YANO S, et al. Molecu-lar design of heat resistant polyimides having excellent processability and high glass transition temperature[J]. High Performance Polymers, 2001, 13(2):S61-S72.

[36]

OGASAWARA T, ISHIKAWA T, YOKOTA R, et al. Processing and properties of carbon fiber reinforced triple-a polyimide (Tri-a PI) matrix composites[J]. Advanced Composite Materials, 2002, 11(3):277-286.

[37]

OGASAWARA T, ISHIDA Y, YOKOTA R, et al. Pro-cessing and properties of carbon fiber/Triple-a polyimide composites fabricated from imide oligomer dry prepreg[J]. Composites Part A, 2007, 38(5):1296-1303.

[38]

LINCOLN J E, MORGAN R J, CURLISS D B. Effect of matrix chemical structure on the thermo-oxidative stabil-ity of addition cure poly(imide siloxane) composites[J]. Polymer Composites, 2008, 29(6):585-596.

[39]

LINCOLN J E, HOUT S, FLAHERTY K, et al. High temperature organic/inorganic addition cure polyimide composites,part 1:matrix thermal properties[J]. Journal of Applied Polymer Science, 2008, 107(6):3557-3567.

[40]

CHENG S L, HAN J H, WANG X, et al. Oxidatively sta-ble thermosets derived from thermal copolymerization of acetylene-terminated imide monomer with an acetylenic monomer containing carborane[J]. Polymer, 2017, 115: 96-105.

[41]

XING T, ZHANG K. Syntheses of novel soluble carbo-rane polyimides with ultrahigh thermal stability[J]. Poly-mer International, 2015, 64(12):1715-1721.

[42]

OZTURK F, COBANOGLU M, Recent advancements in thermoplastic composite materials in aerospace industry[J]. Journal of Thermoplastic Compos-ite Materials, 2024, 37(9):3084-3116.

[43]

ZEYREK B Y, AYDOGAN B, DILEKCAN E, et al. Review of thermoplastic composites in aerospace indus-try[J]. International Journal on Engineering Technolo-gies and Informatics, 2022, 3:1-6.

[44]

HEATHMAN N, KOIRALA P, YAP T, et al. In situ con-solidation of carbon fiber PAEK via laser-assisted auto-mated fiber placement[J]. Composites Part B, 2023, 249:110405.

[45]

SCHIEL I, RAPS L, CHADWICK A R, et al. An investi-gation of in-situ AFP process parameters using CF/LM-PAEK[J]. Advanced Manufacturing, 2020, 6(4) : 191-197.

[46]

KRUEGER R, BERGAN A. Advances in thermoplastic composites over three decades: a literature review: NASA/TM-20240005376[R]. 2024.

[47]

周冰洁, 张代军, 张英杰, . 高性能热塑性复合材料在航空发动机短舱上的应用[J]. 航空制造技术, 2020, 63(7):86-91.

[48]

ZHOU B J, ZHANG D J, ZHANG Y J, et al. Applica-tions of thermoplastic composites on aero-engine nacelles[J]. Aeronautical Manufacturing Technology, 2020, 63(7):86-91.

[49]

王成博, 查萌, 张代军, . 连续碳纤维增强聚芳醚酮热塑性复合材料在航空领域的研究及应用进展[J]. 复合材料学报, 2026, 43(5):2606-2631.

[50]

WANG C B, ZHA M, ZHANG D J, et al. Research and application progress of continuous carbon fiber rein-forced polyaryletherketone thermoplastic composites in the aviation field[J]. Acta Materiae Compositae Sinica. 2026, 43(5):2606-2631.

[51]

燕吉强, 谢宗佑, 李军, . 铺层角度对聚酰亚胺纤维增强复合材料抗高速冲击性能影响[J]. 复合材料科学与工程, 2024(9):12-18.

[52]

YAN J Q, XIE Z Y, LI J, et al. Effect of ply angle on anti-high speed impact properties of polyimide fiber rein-forced composites[J]. Composites Science and Engineer-ing, 2024(9):12-18.

[53]

邹齐, 王乐天, 李军, . 核壳粒子增韧改性液态成型双马树脂性能及其机理[J]. 科技导报, 2023, 41(9):43-50.

[54]

ZOU Q, WANG L T, LI J, et al. Properties and mecha-nism of core-shell particle toughening liquid molding bis-maleimide resin[J]. Science & Technology Review, 2023, 41(9):43-50.

[55]

顾善群, 张代军, 刘燕峰, . 聚酰亚胺纤维/双马树脂复合材料抗高速冲击性能[J]. 材料工程, 2021, 49(1): 119-125.

[56]

GU S Q, ZHANG D J, LIU Y F, et al. Anti-high speed impact properties of polyimide fiber/bismaleimide resin composites[J]. Journal of Materials Engineering, 2021, 49(1):119-125.

[57]

顾善群, 张代军, 付善龙, . 碳纤维/双马树脂复合材料抗高速冲击性能[J]. 材料工程, 2021, 49(11):73-82.

[58]

ZHANG D J, FU S L, et al. Anti-high speed impact properties of carbon fiber/bismaleimide resin com-posites[J]. Journal of Materials Engineering, 2021, 49(11):73-82.

[59]

张代军, 邢宇, 包建文, . 环氧树脂交联结构对固化动力学的影响[J]. 复合材料科学与工程, 2021(7):93-98.

[60]

HANG D J, XING Y, BAO J W, et al. The effect of cross-linked structure of epoxy resin on curing kinetics[J]. Composites Science and Engineering, 2021(7):93-98.

[61]

张代军, 陈俊, 包建文, . 树脂基体中热塑性树脂含量对碳纤维环氧复合材料压缩性能的影响[J]. 复合材料科学与工程, 2021(5):31-36.

[62]

ZHANG D J, CHEN J, BAO J W, et al. Effects of ther-moplastic resin content on longitudinal compressive per-formance of carbon fiber reinforced epoxy compo-sites[J]. Composites Science and Engineering, 2021(5):31-36.

[63]

张代军, 陈俊, 包建文, . 树脂基体中热塑性树脂含量对碳纤维环氧复合材料Ⅱ型层间断裂韧性的影响[J]. 材料工程, 2021, 49(6):178-184.

[64]

ZHANG D J, CHEN J, BAO J W, et al. Effects of ther-moplastic resin content on mode-Ⅱ interlaminar fracture toughness of carbon fiber reinforced epoxy composite[J]. Journal of Materials Engineering, 2021, 49(6):178-184.

[65]

张代军, 包建文, 钟翔屿, . 聚醚砜超细纤维无纺布层间增韧碳纤维/环氧树脂复合材料制备与表征[J]. 复合材料学报, 2022, 39(8):3767-3775.

[66]

ZHANG D J, BAO J W, ZHONG X Y, et al. Preparation and properties of carbon fiber reinforced epoxy resin composites interlaminate-toughened by polyethersulfone ultrafine-fiber non-woven fabric[J]. Acta Materiae Com-positae Sinica, 2022, 39(8):3767-3775.

[67]

ZOU Q, XIAO F, GU S Q, et al. Toughening of bis-maleimide resin based on the self-assembly of flexible aliphatic side chains[J]. Industrial & Engineering Chem-istry Research, 2019, 58(36):16526-16531.

[68]

XING Y, NI H J, ZHANG D J, et al. Strategy construc-tion to improve the thermal resistance of polyimide-matrix composites based on fiber-resin compatibility[J]. Materials, 2025, 18(24):5685.

[69]

倪洪江, 邢宇, 戴霄翔, . 黏度可控化制备 BPDA-PDA 型聚酰亚胺及表征[J]. 材料工程, 2019, 47(11):100-106.

[70]

NI H J, XING Y, DAI X X, et al. Viscosity-controllable preparation and characterization of BPDA-PDA poly-imide[J]. Journal of Materials Engineering, 2019, 47(11):100-106.

[71]

倪洪江, 邢宇, 戴霄翔, . 航空发动机用聚酰亚胺树脂基复合材料固化工艺及热稳定性能[J]. 材料工程, 2022, 50(7):102-109.

[72]

NI H J, XING Y, DAI X X, et al. Curing process and thermal stability of polyimide-matrix composite for aero-engines[J]. Journal of Materials Engineering, 2022, 50(7):102-109.

[73]

倪洪江, 宋恪淳, 李军, . 预置缺陷聚酰亚胺复合材料制备及高温承载性能研究[J]. 复合材料学报, 2025, 42(10):5680-5689.

[74]

NI H J, SONG K C, LI J, et al. Preparation and high tem-perature load-carrying performance of polyimide compos-ites with embedded defects[J]. Acta Materiae Composi-tae Sinica, 2025, 42(10):5680-5689.

[75]

倪洪江, 李军, 邢宇, . 基体厚向梯度化聚酰亚胺复合材料制备与表征[J]. 航空材料学报, 2022, 42(3):55-62.

[76]

NI H J, LI J, XING Y, et al. Preparation and characteriza-tion of matrix-graded polyimide composite along thick-ness direction[J]. Journal of Aeronautical Materials, 2022, 42(3):55-62.

[77]

倪洪江, 李军, 邢宇, . 航空发动机用 T800 级碳纤维增强聚酰亚胺复合材料制备及性能[J]. 复合材料科学与工程, 2022(5):46-51.

[78]

NI H J, LI J, XING Y, et al. Preparation and properties of T800-class carbon fiber reinforced polyimide composite for aero engine[J]. Composites Science and Engineer-ing, 2022(5):46-51.

[79]

张嘉阳, 倪洪江, 龚明, . 表面改性自金属化技术制备表面导电热固性聚酰亚胺复合材料[J]. 复合材料学报, 2021, 38(10):3247-3254.

[80]

ZHANG J Y, NI H J, GONG M, et al. Preparation of sur-face conductive thermosetting polyimide composites by surface modification self-metallization process[J]. Acta Materiae Compositae Sinica, 2021, 38(10):3247-3254.

[81]

ZHANG J Y, NI H J, GONG M, et al. Realization of electromagnetic shielding performance for polyimide-matrix composite by self-metallization[J]. Journal of Composite Materials, 2021, 55(26):3849-3860.

[82]

付善龙, 雷帅, 李军, . 航空用国产碳纤维/聚酰亚胺复合材料耐环境老化性能[J]. 热固性树脂, 2023, 38(4):1-6.

[83]

FU S L, LEI S, LI J, et al. Environmental aging resis-tance of domestic carbon fiber/polyimide composites for aviation[J]. Thermosetting Resin, 2023, 38(4):1-6.

[84]

方文宇, 倪洪江, 龚明, . 高温热老化对聚酰亚胺复合材料性能的影响[J]. 塑料科技, 2025, 53(7):14-18.

[85]

FANG W Y, NI H J, GONG M, et al. Effect of high tem-perature thermal aging on properties of polyimide com-posites[J]. Plastics Science and Technology, 2025, 53(7):14-18.

[86]

邢宇, 张代军, 王成博, . PEEK 复合材料用碳纤维上浆剂研究进展[J]. 材料工程, 2022, 50(8):70-81.

[87]

XING Y, ZHANG D J, WANG C B, et al. Research progress in carbon fiber sizing agents for PEEK compos-ites[J]. Journal of Materials Engineering, 2022, 50(8): 70-81.

[88]

王成博, 张代军, 关博文, . 基于自动铺放技术的聚芳醚酮复合材料后处理工艺优化[J]. 航空材料学报, 2025, 45(3):32-42.

[89]

WANG C B, ZHANG D J, GUAN B W, et al. Optimiza-tion of post-processing of PAEK composites based on automated placement technology[J]. Journal of Aeronau-tical Materials, 2025, 45(3):32-42.

[90]

王成博, 张代军, 李军, . 碳纤维高温气相氧化对聚醚醚酮复合材料拉伸和层间剪切性能的影响[J]. 复合材料学报, 2024, 41(12):6425-6437.

[91]

WANG C B, ZHANG D J, LI J, et al. Effect of high-tem-perature gas-phase oxidation of carbon fiber on tensile and interlaminar shear properties of PEEK compo-sites[J]. Acta Materiae Compositae Sinica, 2024, 41(12):6425-6437.

[92]

叶璐, 张代军, 李军, . 碳纤维增强聚芳醚酮热塑性复合材料电阻焊接工艺研究[J]. 复合材料科学与工程, 2024(8):45-52.

[93]

YE L, ZHANG D J, LI J, et al. Research on resistance welding technology of carbon fiber reinforced polyaryl ether ketone thermoplastic composites[J]. Composites Science and Engineering, 2024(8):45-52.

[94]

叶璐, 张代军, 李军, . 热塑性复合材料电阻焊接技术研究进展[J]. 航空材料学报, 2025, 45(3):19-31.

[95]

YE L, ZHANG D J, LI J, et al. Research progress in resistance welding technology of thermoplastic compos-ites[J]. Journal of Aeronautical Materials, 2025, 45(3): 19-31.

[96]

李杰. GE 公司复合材料风扇叶片的发展和工艺[J]. 航空发动机, 2008, 34(4):54-55.

[97]

LI J. Development and technology for complex material fan blade of GE[J]. Aeroengine, 2008, 34(4):54-55.

[98]

De LUYCKER E, MORESTIN F, BOISSE P, et al. Sim-ulation of 3D interlock composite preforming[J]. Com-posite Structures, 2009, 88(4):615-623.

[99]

WILSON D. PMR-15 processing, properties and prob-lems: a review[J]. British Polymer Journal, 1988, 20(5):405-416.

[100]

刘超, 吴正洪, 邵红艳, . 树脂基复合材料外涵机匣结构设计与试验验证[J]. 复合材料科学与工程, 2022(6):81-88.

[101]

LIU C, WU Z H, SHAO H Y, et al. Structure design and verification of resin matrix composite bypass casing[J]. Composites Science and Engineering, 2022(6):81-88.

[102]

汪存显. 复合材料发动机机匣包容性机理研究[D]. 西安: 西北工业大学, 2019.

[103]

WANG C X. Investigation on mechanism of containment for composites engine casing[D]. Xi’an: Northwestern Polytechnical University, 2019.

[104]

WEI J H, ZHANG Y F, LIU Y F, et al. Advances in resin matrix composite fan blades for aircraft engines: a review[J]. Thin-Walled Structures, 2024, 202:112058.

[105]

MARSH G. Aero engines lose weight thanks to compos-ites[J]. Reinforced Plastics, 2012, 56(6):32-35.

基金资助

国家科技重大专项(2017-Ⅷ-0011)

国家科技重大专项(J2019-Ⅵ-0013)

AI Summary AI Mindmap
PDF (3177KB)

0

访问

0

被引

详细

导航
相关文章

AI思维导图

/