Methods for fabrication of layups for composite honeycomb core sandwich structures and said composite honeycomb core sandwich structures
AssigneeThe Boeing Company
InventorsKevin L. Robbins, Marc G. Storozuk
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AssigneeThe Boeing Company
InventorsKevin L. Robbins, Marc G. Storozuk
Estimating the term…
A method for fabrication of a layup for a composite honeycomb core sandwich structure includes laying up a first plurality of unidirectional tows over a tool for layup of the composite honeycomb core sandwich structure using an automated fiber placement process to form a stack of under-core composite plies that are tied down to a rough textured surface bonded to the tool; placing a honeycomb core on the stack of under-core composite plies within the rough textured surface; and laying up a second plurality of unidirectional tows over the honeycomb core using the automated fiber placement process to form a stack of over-core composite plies that tie down the honeycomb core to the rough textured surface. The method may also include placing an under-core film adhesive on the stack of under-core composite plies and placing an over-core film adhesive on the honeycomb core.
A method for fabrication of a layup for a composite honeycomb core sandwich structure, the method comprising:
A method for fabrication of a layup for a composite honeycomb core sandwich structure, the method comprising:
Dependencies are inferred from the claim text.