试验研究了用于航空结构的三维整体编织复合材料单耳承力接头在静载条件下的承载能力与破坏模式。单耳接头试样采用RTM(Resin Transfer Molding树脂传递模塑)工艺制成,重点研究了由3种编织工艺(三维四向、三维五向和三维六向)、2种连接...试验研究了用于航空结构的三维整体编织复合材料单耳承力接头在静载条件下的承载能力与破坏模式。单耳接头试样采用RTM(Resin Transfer Molding树脂传递模塑)工艺制成,重点研究了由3种编织工艺(三维四向、三维五向和三维六向)、2种连接孔加工方式(机械钻孔和编织孔)、2种几何外形所组成的10组三维编织复合材料单耳承力接头的破坏机理与破坏载荷。对其在航空结构中的可应用性做出了评估。展开更多
The yarn architecture of 3-D braided composites products by the four-step 1×1 braiding technique has been studied by means of a control volume method in conjunction with experimental investigation and a numerical...The yarn architecture of 3-D braided composites products by the four-step 1×1 braiding technique has been studied by means of a control volume method in conjunction with experimental investigation and a numerical method, respectively. An ellipse assumption for the cross-section of yarn was proposed in this analysis method with considering the yarn size and yarn-packing factor. Two types of local unit cell structures were identified for 4-step braided composites by considering the nature of the braiding processes and by observing the sample cross-sections. The relationship between the braiding procedure and the properties for 3-D braided structural shapes was established. This method provides the basis for analyzing stiffness and strength of 3-D braided composites.展开更多
文摘试验研究了用于航空结构的三维整体编织复合材料单耳承力接头在静载条件下的承载能力与破坏模式。单耳接头试样采用RTM(Resin Transfer Molding树脂传递模塑)工艺制成,重点研究了由3种编织工艺(三维四向、三维五向和三维六向)、2种连接孔加工方式(机械钻孔和编织孔)、2种几何外形所组成的10组三维编织复合材料单耳承力接头的破坏机理与破坏载荷。对其在航空结构中的可应用性做出了评估。
基金Aeronautical Science Foundation of China ( 99B2 3 0 0 1)
文摘The yarn architecture of 3-D braided composites products by the four-step 1×1 braiding technique has been studied by means of a control volume method in conjunction with experimental investigation and a numerical method, respectively. An ellipse assumption for the cross-section of yarn was proposed in this analysis method with considering the yarn size and yarn-packing factor. Two types of local unit cell structures were identified for 4-step braided composites by considering the nature of the braiding processes and by observing the sample cross-sections. The relationship between the braiding procedure and the properties for 3-D braided structural shapes was established. This method provides the basis for analyzing stiffness and strength of 3-D braided composites.
