宇航材料工艺
宇航材料工藝
우항재료공예
AEROSPACE MATERIALS & TECHNOLOGY
2010年
1期
86-89
,共4页
李勇%肖军%原永虎%谭永刚
李勇%肖軍%原永虎%譚永剛
리용%초군%원영호%담영강
夹层结构%X-cor%Pin%平拉试验
夾層結構%X-cor%Pin%平拉試驗
협층결구%X-cor%Pin%평랍시험
Sandwich structures%X-cor%Pin%Flatwise tensile testing
研究了Pin植入角、Pin直径和Pin材料对X-cor夹层结构平拉强度及平拉模量的影响.平拉性能试样采用Rohacell 31泡沫作为芯材,Pin采用不同直径的T300/FW-63和SC-240/FW-63拉挤细杆.结果表明,X-cor夹层结构平拉强度增强效率随着植入角度的增加先增大、后减小,平拉模量的增强效率则随植入角的增加而减小;随Pin直径减小,平拉强度增强效率增加,平拉模量增强效率降低;不同Pin材料对X-cor夹层结构平拉强度增强效率相同,高模量的Pin对X-cor夹层结构平拉模量的增强效率更高.
研究瞭Pin植入角、Pin直徑和Pin材料對X-cor夾層結構平拉彊度及平拉模量的影響.平拉性能試樣採用Rohacell 31泡沫作為芯材,Pin採用不同直徑的T300/FW-63和SC-240/FW-63拉擠細桿.結果錶明,X-cor夾層結構平拉彊度增彊效率隨著植入角度的增加先增大、後減小,平拉模量的增彊效率則隨植入角的增加而減小;隨Pin直徑減小,平拉彊度增彊效率增加,平拉模量增彊效率降低;不同Pin材料對X-cor夾層結構平拉彊度增彊效率相同,高模量的Pin對X-cor夾層結構平拉模量的增彊效率更高.
연구료Pin식입각、Pin직경화Pin재료대X-cor협층결구평랍강도급평랍모량적영향.평랍성능시양채용Rohacell 31포말작위심재,Pin채용불동직경적T300/FW-63화SC-240/FW-63랍제세간.결과표명,X-cor협층결구평랍강도증강효솔수착식입각도적증가선증대、후감소,평랍모량적증강효솔칙수식입각적증가이감소;수Pin직경감소,평랍강도증강효솔증가,평랍모량증강효솔강저;불동Pin재료대X-cor협층결구평랍강도증강효솔상동,고모량적Pin대X-cor협층결구평랍모량적증강효솔경고.
To experimentally study the influence of pin' s angle and diameter and pin materials on the strength and modulus of X-cor sandwich structures, the specimens of flatwise tensile test were made of the Rohacell 31 foam core and the pins with different kinds of diameter consisting of T300/FW-63 carbon/epoxy and SC-240/FW-63 glass/ epoxy with pultrusion process. The results show that the efficiency of pin reinforcing flatwise tensile strength of X-cor sandwich structures increased first and then decreased as pin's angle increased and increased as pin's diameter de-creased, the efficiency of pin reinforcing flatwise tensile modulus of X-cor sandwich structures decreased as pin's an-gle increased and decreased as pin's diameter decreased, the efficiency of pin reinforcing flatwise tensile strength of X-cor sandwich structures is keep constant with different pins materials, but the efficiency of pin reinforcing flatwise tensile modulus of X-cor sandwich structures is higher with higher modulus pins.