2009
DOI: 10.1016/j.compositesa.2009.02.012
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A concept to optimize quality and cost in thermoplastic composite components applied to the production of helicopter canopies

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Cited by 34 publications
(49 citation statements)
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“…The present study explores alternative manufacturing and recycling scenarios in terms of financial and environmental viability, associated with the canopy of the EUROCOPTER EC Twin Star helicopter described in [3]. The canopy is assumed to be made of a carbon fiber reinforced epoxy composite material, with a 60% fiber volume fraction.…”
Section: Definition Of the Case Studymentioning
confidence: 99%
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“…The present study explores alternative manufacturing and recycling scenarios in terms of financial and environmental viability, associated with the canopy of the EUROCOPTER EC Twin Star helicopter described in [3]. The canopy is assumed to be made of a carbon fiber reinforced epoxy composite material, with a 60% fiber volume fraction.…”
Section: Definition Of the Case Studymentioning
confidence: 99%
“…The canopy is assumed to be made of a carbon fiber reinforced epoxy composite material, with a 60% fiber volume fraction. The total mass of the canopy was calculated based on [3] and found equal to 0,64 kg. As a result the mass of the carbon fibers and the epoxy were found equal to 0,384 kg and 0,256 kg respectively.…”
Section: Definition Of the Case Studymentioning
confidence: 99%
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