Cutting wire for removal of expanded material after curing of a composite part
AssigneeThe Boeing Company
InventorsGary E. Georgeson, Xiaoxi Wang, Jonathan Santiago
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AssigneeThe Boeing Company
InventorsGary E. Georgeson, Xiaoxi Wang, Jonathan Santiago
Estimating the term…
Composite fabrication system and associated methods. In one embodiment, a composite fabrication system comprises a molding tool that includes a forming surface at least partially disposed within a constrained space, and a foamable material that expands inside of the constrained space to form an expanded material that presses a layup of one or more composite layers against the molding tool. The composite fabrication system further comprises a curing device configured to cure the layup to form a composite part, and a cutting wire embedded in the constrained space that is heated and configured to cut the expanded material into pieces that are removable from the constrained space.
A method of fabricating a composite part, the method comprising:
A composite fabrication system, comprising:
A method of fabricating a composite part, the method comprising:
Dependencies are inferred from the claim text.