大型民用飛機(jī)復(fù)合材料結(jié)構(gòu)的經(jīng)驗(yàn)總結(jié)之一：碳纖維增強(qiáng)復(fù)合材料的抗壓強(qiáng)度研究

主講人 : 牛康民 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(jiǎn)介：

?？得?，北京科技大學(xué)退休教授、博導(dǎo)、杰出學(xué)者、國(guó)家特聘專家；前任北科大復(fù)合材料結(jié)構(gòu)工程中心主任；此前任西門子公司院士工程師，負(fù)責(zé)新一代大型燃?xì)廨啓C(jī)葉片完整性和壽命方法包括高性能碳纖維樹(shù)脂基復(fù)合材料和陶瓷基復(fù)合材料結(jié)構(gòu)。曾任美國(guó)波音公司機(jī)體結(jié)構(gòu)實(shí)驗(yàn)室結(jié)構(gòu)技術(shù)負(fù)責(zé)人，做為波音民用飛機(jī)集團(tuán)復(fù)合材料結(jié)構(gòu)資深專家參與了最新型777X、787夢(mèng)想飛機(jī)機(jī)翼和機(jī)身結(jié)構(gòu)的設(shè)計(jì)、分析與試驗(yàn)。主導(dǎo)確立公司非線性有限元模型分析方法。佐治亞理工大學(xué) Georgia Institute of Technology 航空工程博士。