Fastener insert for a composite sandwich panel, a panel assembly, and a method of fastening a component to a composite sandwich panel
AssigneeThe Boeing Company
InventorChristopher J. Mills
Life of this patent
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AssigneeThe Boeing Company
InventorChristopher J. Mills
Estimating the term…
A fastener insert for securement to a composite sandwich panel at an opening in the composite sandwich panel includes a base and a fastener carrier. The base has a body and a flange integral with the body. The flange extends laterally outward of an outer perimeter of the body. The base defines a central cavity extending entirely through both the body and the flange. The base includes a first locking feature disposed at the central cavity. The fastener carrier is configured to insert into the central cavity of the base. The fastener carrier defines a fastener opening and has a second locking feature configured for mechanical engagement with the first locking feature of the base to retain the fastener carrier to the base. A panel assembly and a method of fastening a component to a composite sandwich panel utilize the fastener insert.
A fastener insert for securement to a composite sandwich panel at an opening in the composite sandwich panel, the fastener insert comprising:
A panel assembly comprising:
A method of fastening a component to a composite sandwich panel, the composite sandwich panel including a core, a first skin covering one side of the core at a first side of the composite sandwich panel, and a second skin covering an opposing side of the core at a second side of the composite sandwich panel, the method comprising:
Dependencies are inferred from the claim text.