AXIAL COMPOSITE MEMBER AND MANUFACTURING METHOD THEREFOR

PROBLEM TO BE SOLVED: To improve durability by securing desired strength of a bent part.SOLUTION: A bent part of an axial member 10 is formed by laminating 0° layers 16 in which the orientation direction of a carbon fiber is parallel to the axial direction of the axial composite member 10, and ±45°...

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Bibliographic Details
Main Authors KIYOMOTO HIROSHI, TANEDA KAZUHIRO, YAMADA NOBUHIRO
Format Patent
LanguageEnglish
Japanese
Published 05.09.2016
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Summary:PROBLEM TO BE SOLVED: To improve durability by securing desired strength of a bent part.SOLUTION: A bent part of an axial member 10 is formed by laminating 0° layers 16 in which the orientation direction of a carbon fiber is parallel to the axial direction of the axial composite member 10, and ±45° layers 18 in which the orientation direction of the carbon fiber is obliquely intersected with the axial direction of the axial composite member 10, and further a stress relaxation layer 20 is interposed between the 0° layers and the ±45° layers. The stress relaxation layer 20 is set to be lower than bending rigidity of the 0° layer and lower than torsional rigidity of the ±45° layer.SELECTED DRAWING: Figure 3 【課題】曲げ部の所望の強度を確保して耐久性を向上させること。【解決手段】軸状部材10の曲げ部は、外径側に位置し、炭素繊維の配向方向が軸状複合部材10の軸方向に対して平行な0°層16と、内径側に位置し、炭素繊維の配向方向が軸状複合部材10の軸方向に対して斜交する±45°層18とが積層して形成され、さらに、0°層と±45°層との間には、応力緩和層20が介装され、応力緩和層20は、0°層の曲げ剛性よりも低く、且つ、±45°層の捩り剛性よりも低く設定される。【選択図】図3
Bibliography:Application Number: JP20150041159