Composite ply stabilizing system
AssigneeThe Boeing Company
InventorsDoan D. Pham, Mark W. Tollan, Richard M. Outzen, John C. Lockleer, Christopher G. Harris
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AssigneeThe Boeing Company
InventorsDoan D. Pham, Mark W. Tollan, Richard M. Outzen, John C. Lockleer, Christopher G. Harris
Estimating the term…
A stabilizing mechanism for resisting relative movement of upper and lower laminates of a composite structure having a core comprises a lower grip strip and at least one upper grip strip. The lower grip strip may be mounted to a tool upon which the composite structure may be processed. The lower grip strip may include an outer surface having at least one engagement feature for engaging at least one of the upper and lower laminates which make up the composite structure. The upper grip strip may have opposing outer surfaces which may include at least one engagement feature for engaging the lower strip and at least one of the upper and lower laminates.
A stabilizing mechanism for resisting relative movement of upper and lower laminates of a composite structure having a core, the stabilizing mechanism comprising:
A stabilizing mechanism for resisting relative movement of upper and lower laminates mounted to a chamfered core of a composite structure to prevent core crush of the chamfered core under the application of autoclave force to the chamfered core, the upper and lower laminates being respectively mounted to upper and lower surfaces of the core, the upper and lower laminates being respectively comprised of upper and lower plies, the composite structure having a perimeter including a trim line defining a trim margin, the stabilizing mechanism comprising:
A system for resisting relative movement of upper and lower laminates mounted to a chamfered core of a composite structure to reduce core crush of the chamfered core, the system comprising:
Dependencies are inferred from the claim text.