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US 11,685,509 B2Granted
Integrally stiffened bonded panel with vented pockets and methods of manufacture
AssigneeThe Boeing Company
InventorsDavid M. Anderson, Jeffrey P. Baucum
Life of this patent
Estimating the term…
Abstract
Methods, systems, and apparatuses are disclosed for the manufacture of composite components having incorporated reinforcing structures machined into composite material substrates, and composite components manufactured according to disclosed methods, and assemblies and larger structures comprising the composite material components.
Claims13
A method for forming a composite material component, said method comprising:
- orienting a plurality of composite material layers onto a tool to form a first composite material substrate, said first composite material substrate comprising a first composite material substrate thickness, said tool comprising a tooling surface, and said first composite material substrate further comprising:
- a first composite material substrate first surface, said first composite material substrate first surface positioned in contact with the tooling surface;
- a first composite material substrate second surface, said first composite material substrate second surface comprising an inner mold line;
- providing a second composite material substrate to the first composite material substrate second surface, said second composite material substrate comprising a second composite material substrate first surface and a second composite material substrate second surface, said second composite material substrate first surface configured to contact said first composite material substrate second surface;
- imparting said inner mold line from the first composite material substrate second surface to said second composite material substrate first surface;
- removing said second composite material substrate from said first composite material substrate second surface;
- at least partially curing the first composite material substrate;
- machining a plurality of recesses into the first composite material substrate second surface, said plurality of recesses configured to extend from the first composite material second surface to a predetermined distance into the first composite material substrate thickness to form a machined composite material substrate, said machined composite material substrate comprising a machined composite material substrate first surface and a machined composite material substrate second surface, said plurality of recesses each comprising a recess perimeter at the machined composite substrate material second surface;
- machining at least one channel into the first composite material substrate second surface, said at least one channel configured to intersect a plurality of recesses;
- orienting the second composite material substrate first surface onto the machined composite material substrate second surface;
- bonding the second composite material substrate first surface to the machined composite material substrate second surface to form a composite material component, said composite material component comprising at least one internal pathway;
- wherein said at least one internal pathway is bounded by the machined composite material substrate and the second composite material substrate first surface;
- and
- wherein said at least one internal pathway comprises a plurality of interconnected recesses.
11 more elements
Dependencies are inferred from the claim text.