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Flexural rigidity evolvement laws of reinforced concrete beams strengthened with carbon fiber laminates
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作者 牛鹏志 《Journal of Chongqing University》 CAS 2007年第1期67-72,共6页
Extensive research has shown that externally bonded carbon fiber reinforced polymer (CFRP) laminates are particularly suitable for improving the fatigue behavior of reinforced concrete (RC) beams. This paper prese... Extensive research has shown that externally bonded carbon fiber reinforced polymer (CFRP) laminates are particularly suitable for improving the fatigue behavior of reinforced concrete (RC) beams. This paper presents the research on flexural ngidity evolvement laws by testing 14 simple-supported RC beams strengthened with carbon fiber laminates (CFL) under cyclic load, and 2 under monotone load as a reference. The cyclic load tests revealed the peak load applied onto the surface of a supported RC beam strengthened with CFL is linear to the logarithm of its fatigue life, and the flexural rigidity evolvement undergoes three distinct phases: a rapid decrease from the start to about 5% of the fatigue life; an even development from .5% to about 99% of the fatigue life; and a succedent rapid decrease to failure. When the ratio of fatigue "cycles to the fatigue life is within 0.0.5 to 0.99, the flexural rigidity varies linearly with the ratio. The peak load does not affect the flexural rigidity evolvement if it is not high enough to make the main reinforcements yield. The dependences of the flexural rigidity of specimens formed in the same group upon their fatigue cycles normalized by fatigue life are almost coincident. This implies the flexural rigidity may be a material parameter independent of the stress level. These relationships of flexural rigidity to fatigue cycles, and fatigue life may be able to provide some hints for fatigue design and fatigue life evaluation of RC member strengthened with CFL; nevertheless the findings still need verifying by more experiments. 展开更多
关键词 flexural rigidity carbon fiber laminate reinforced concrete BEAM FATIGUE
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左支架多工位级进模的设计 被引量:1
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作者 武晓红 《锻压技术》 CAS CSCD 北大核心 2022年第12期189-192,共4页
为了解决成形高度大且含有密集的局部成形的制品在成形时的材料开裂问题,采用了预成形、预冲孔、再成形,最后整形的多次成形方法。成形结果表明,局部成形高度可达材料厚度的8倍,制品在生产中没有出现开裂现象,产品质量稳定。为了解决小... 为了解决成形高度大且含有密集的局部成形的制品在成形时的材料开裂问题,采用了预成形、预冲孔、再成形,最后整形的多次成形方法。成形结果表明,局部成形高度可达材料厚度的8倍,制品在生产中没有出现开裂现象,产品质量稳定。为了解决小凸模易折断的问题,采用了护套固定小凸模的结构,明显提高了小凸模的寿命。为了解决弯曲回弹问题,采用了减少弯曲凸模与材料接触面积的凸模结构,该结构可增大弯曲区的压应力,达到减少弯曲回弹的目的。左支架级进模成形的工件完全符合产品的质量要求,模具的维修率低。该模具的成功投产表明:采用预冲孔和多次成形相结合的措施,能够有效地提高带孔凸包的成形高度,防止材料开裂。 展开更多
关键词 级进模 局部成形 压加强筋 凸包 护套固定小凸模 弯曲回弹
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