COMPARISON OF ENERGY-ABSORPTION OF CARBON EPOXY AND CARBON PEEK COMPOSITE TUBES

被引:109
作者
HAMADA, H
COPPOLA, JC
HULL, D
MAEKAWA, Z
SATO, H
机构
[1] UNIV CAMBRIDGE,DEPT MAT SCI & MET,PEMBROKE ST,CAMBRIDGE CB2 3QZ,ENGLAND
[2] KYOTO INST TECHNOL,FAC FIBRE SCI,SAKYO KU,KYOTO 606,JAPAN
[3] YOKOHAMA RUBBER CO LTD,DIV ADV COMPOSITE MAT,HIRATSAKA CITY,KANAGAWA 254,JAPAN
来源
COMPOSITES | 1992年 / 23卷 / 04期
关键词
COMPOSITE MATERIALS; TUBES; AXIAL COMPRESSION; SPECIFIC ENERGY ABSORPTION; FIBER ARCHITECTURE; CHAMFER TRIGGER; CRUSH ZONE MORPHOLOGY; CARBON FIBERS; EPOXY; PEEK;
D O I
10.1016/0010-4361(92)90184-V
中图分类号
TB33 [复合材料];
学科分类号
摘要
Axial compressive tests have been carried out on carbon fibre/epoxy and carbon fibre/PEEK tubes made from unidirectional prepreg materials. Three fibre architectures were investigated: unidirectional fibres parallel (0-degrees) to the axis of the tube, +/-30-degrees and +/-45-degrees. One set of tubes was machined with a 45-degrees chamfer at one end in an attempt to trigger progressive crushing and the other set had square ends to determine the compressive strength of the material. Stable progressive crushing occurred in +/-45-degrees carbon fibre/epoxy tubes and 0-degrees carbon fibre/PEEK tubes where the crush stress was significantly lower than the compressive fracture strength. The 0-degrees carbon fibre/PEEK tubes had a specific energy absorption of 180 kJ kg-1, which is the highest value recorded for any material. This high value is interpreted in terms of the high interlaminar toughness of PEEK-matrix composites.
引用
收藏
页码:245 / 252
页数:8
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