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    Using Embossing to Create a Fiber Reinforced Honeycomb Composite

    Source: Journal of Engineering Materials and Technology:;2005:;volume( 127 ):;issue: 002::page 257
    Author:
    William Jordan
    DOI: 10.1115/1.1867985
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This research project used hot embossing to create a strong and tough polymeric based composite structure. A honeycomb type structure was created by pressing small grooves into thin polycarbonate sheets. A trapezoidal die was used to create hexagonal shaped channels in the polymeric sheet. A number of these sheets were then bonded together to form a composite material. Carbon fibers were embedded into the channels in some of the laminates. The embossing process was carried out at an elevated temperature in an environmental chamber attached to an MTS servo hydraulic testing machine. The grooved structure had a 31% to 45% decrease in the apparent density compared to the ungrooved specimens. Bend tests, tensile tests, and Charpy impact tests were performed on laminates made from this material. The specific values of tensile strength, flexural modulus, and Charpy impact toughness were increased. A small percentage of fibers significantly increased both the stiffness and strength of the laminate.
    keyword(s): Composite materials , Fibers , Laminates , Embossing , Temperature , Channels (Hydraulic engineering) AND Toughness ,
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      Using Embossing to Create a Fiber Reinforced Honeycomb Composite

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    http://yetl.yabesh.ir/yetl1/handle/yetl/131889
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    contributor authorWilliam Jordan
    date accessioned2017-05-09T00:16:18Z
    date available2017-05-09T00:16:18Z
    date copyrightApril, 2005
    date issued2005
    identifier issn0094-4289
    identifier otherJEMTA8-27070#257_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131889
    description abstractThis research project used hot embossing to create a strong and tough polymeric based composite structure. A honeycomb type structure was created by pressing small grooves into thin polycarbonate sheets. A trapezoidal die was used to create hexagonal shaped channels in the polymeric sheet. A number of these sheets were then bonded together to form a composite material. Carbon fibers were embedded into the channels in some of the laminates. The embossing process was carried out at an elevated temperature in an environmental chamber attached to an MTS servo hydraulic testing machine. The grooved structure had a 31% to 45% decrease in the apparent density compared to the ungrooved specimens. Bend tests, tensile tests, and Charpy impact tests were performed on laminates made from this material. The specific values of tensile strength, flexural modulus, and Charpy impact toughness were increased. A small percentage of fibers significantly increased both the stiffness and strength of the laminate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUsing Embossing to Create a Fiber Reinforced Honeycomb Composite
    typeJournal Paper
    journal volume127
    journal issue2
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.1867985
    journal fristpage257
    journal lastpage262
    identifier eissn1528-8889
    keywordsComposite materials
    keywordsFibers
    keywordsLaminates
    keywordsEmbossing
    keywordsTemperature
    keywordsChannels (Hydraulic engineering) AND Toughness
    treeJournal of Engineering Materials and Technology:;2005:;volume( 127 ):;issue: 002
    contenttypeFulltext
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