Composite structure and core positioning ply
AssigneeSikorsky Aircraft Corporation
InventorsJonathan Bremmer, Jeffrey G. Sauer, Edward Joseph Fabian, Paul H. Denavit, Darryl Mark Toni, William E. Hovan, III
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AssigneeSikorsky Aircraft Corporation
InventorsJonathan Bremmer, Jeffrey G. Sauer, Edward Joseph Fabian, Paul H. Denavit, Darryl Mark Toni, William E. Hovan, III
Estimating the term…
A composite structure includes a first laminate, a second laminate, and at least one core component located between the first laminate and the second laminate. The at least one core component includes a honeycomb core and at least one locking ply extending from the honeycomb core between the first laminate and the second laminate. The at least one locking ply is configured such that a pressure applied during a cure cycle of the composite structure retains the at least one locking ply between the first laminate and the second laminate thereby preventing movement of core component.
A composite structure comprising:
A method of forming a composite structure comprising:
Dependencies are inferred from the claim text.