Veil-stabilized composite with improved tensile strength
AssigneeThe Boeing Company
InventorThomas K. Tsotsis
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AssigneeThe Boeing Company
InventorThomas K. Tsotsis
Estimating the term…
A method for manufacturing a composite may include: selecting an interlayer material having a first distortional-deformation capability; selecting a matrix material having a second distortional-deformation capability, which is less than the first distortional-deformation capability; disposing at least one reinforcing layer, formed of reinforcing fibers of a reinforcing material, and at least one interlayer, formed of a nonwoven fabric of the interlayer material, in an alternating configuration; and infusing the at least one reinforcing layer and the at least one interlayer with the matrix material such that the matrix material flows though the at least one reinforcing layer and the at least one interlayer. Selection of the interlayer material having the first distortional-deformation capability and the matrix material having the second distortional-deformation capability is configured to increase tensile strength of the composite.
A method for manufacturing a composite, said method comprising:
A method for manufacturing a composite, said method comprising:
A method for improving tensile strength of a composite comprising at least one reinforcing layer, formed of reinforcing fibers of a reinforcing material, and at least one interlayer, formed of a nonwoven fabric of an interlayer material, disposed in an alternating configuration and infused with a matrix material, said method comprising:
Dependencies are inferred from the claim text.