2019
DOI: 10.1007/s12541-019-00265-z
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Design of Prepreg Compression Molding for Manufacturing of CFRTP B-pillar Reinforcement with Equivalent Mechanical Properties to Existing Steel Part

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Cited by 16 publications
(8 citation statements)
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“…Although many CFRTP parts can be manufactured into near-net-shape [8,9], riveting through assembly holes is still indispensable for rapid assembly of load bearing parts [10] and precise positioning of aircraft components [11]. To date, literature on hole making of the well-established conventional thermoset CF/epoxy composites is widely available [12][13][14].…”
Section: Introductionmentioning
confidence: 99%
“…Although many CFRTP parts can be manufactured into near-net-shape [8,9], riveting through assembly holes is still indispensable for rapid assembly of load bearing parts [10] and precise positioning of aircraft components [11]. To date, literature on hole making of the well-established conventional thermoset CF/epoxy composites is widely available [12][13][14].…”
Section: Introductionmentioning
confidence: 99%
“…The process consists of the transformation of a mat preform i.e. a mixture of fiber and resin into the desired product by employing corresponding metal molds [173][174][175]. Figure 19 represents the representative diagram of the key components of a typical compression press [174].…”
Section: Compression Moldingmentioning
confidence: 99%
“…Figure 4 shows the formability evaluation of the B-pillar by comparison with the FLDs under different temperatures [ 20 ]. The temperature of the boron steel decreased during the forming stage owing to the contact between the tool and blank, which could lead to problems, such as cracking and wrinkling.…”
Section: Process Design Of the B-pillar Assembly By Fe Simulationmentioning
confidence: 99%