大型民用飛機復合材料結構的經驗總結之一：碳纖維增強復合材料的抗壓強度研究

主講人 : ?？得?教授

Over the past 50 years, advanced Carbon Fiber Reinforced Polymer (CFRP) composites have become central to large commercial aircraft structures. This paper reviews compressive strength  d on the latest data and results from Toray and provides a comprehensive theoretical investigation into predicting CFRP compressive performance, with a focus on kinking band formation mechanisms.

The findings highlight that the compressive strength of high-performance CFRP composites is primarily determined by the stiffness and toughness of the resin assuming the elimination of bonding defects and fiber misalignments. To advance CFRP materials, enhancing the resin's nonlinear shear modulus should be prioritized. This is especially significant for China’s C919 and C929 projects, which aim to replace imported CFRP with domestically sourced materials, advancing self-reliance in aerospace manufacturing.

主講人簡介：

?？得?，北京科技大學退休教授、博導、杰出學者、國家特聘專家；前任北科大復合材料結構工程中心主任；此前任西門子公司院士工程師，負責新一代大型燃氣輪機葉片完整性和壽命方法包括高性能碳纖維樹脂基復合材料和陶瓷基復合材料結構。曾任美國波音公司機體結構實驗室結構技術負責人，做為波音民用飛機集團復合材料結構資深專家參與了最新型777X、787夢想飛機機翼和機身結構的設計、分析與試驗。主導確立公司非線性有限元模型分析方法。佐治亞理工大學 Georgia Institute of Technology 航空工程博士。