主权项 |
1. A method of making a integral, single composite structure within a tool, the method comprising:
arranging a plurality of pressurizable members within the tool, each of the pressurizable members having a desired shape before pressurization that includes an outer surface and an inner surface defining a volumetric region, each of the pressurizable members further having an opening to permit internal pressurization thereof, wherein at least one of the pressurizable members includes a recessed region, wherein the pressurizable members are coupled together to be in fluid communication with an adjacent pressurizable member, and wherein the pressurizable members substantially maintain their desired shape without requiring an internal support member; arranging a first plurality of fiber plies onto at least one surface of each of the plurality of pressurizable members, wherein at least some of the first fiber plies are placed onto the recessed region to substantially conform therewith; placing a cored member onto the recessed, first fiber plies, the cored member complementarily configured to conform to the recessed region; arranging a second plurality of fiber plies onto the first plurality of fiber plies and onto the cored member to substantially form the composite structure, wherein each of the pressurizable members substantially maintains its respective, desired shape after being loaded with the fiber plies, yet before pressurization thereof; pressurizing an outer surface of the composite assembly with a first pressure; and pressurizing the inner surface of the pressurizable members with a second pressure, wherein the first pressure and the second pressure operate to compress the fiber plies without crushing the cored member, and wherein the fiber ply compression operates to mitigate wrinkle formation. |