Methods and systems for composite structural truss
Methods and structures for a composite truss structure are provided. The structure includes a web formed of a plurality of sheets of composite material, each sheet including a first face and an opposing second face and each face including a length and a width. Each of the plurality of sheets are coupled to at least one other of the plurality of sheets face to face such that the length and width of each face substantially match the length and width of a face of an adjacent sheet. The plurality of sheets are formed to include an upper chord member, a lower chord member, and a plurality of web members extending therebetween. The structure also includes at least a first flange plate coupled to the web proximate an outer periphery of the web.
1. A truss comprising:
a first composite plate structure; and
a second composite plate structure coupled directly to said first composite plate structure to form said truss, wherein each of said first and second composite plate structures comprises:
an upper chord member;
a lower chord member;
a plurality of web members extending between said upper and lower chord members to form at least a portion of an aircraft wing rib; and
a first flange plate formed about an opening defined by at least one portion of said web members and extending perpendicular to said web members, wherein said plurality of web members comprises at least one web member extending obliquely between said upper chord member and said lower chord member, and wherein the opening receives an aft wing spar;
wherein said first composite plate structure first flange plate and said second composite plate structure first flange plate extend away from one another and are separated from one another by a gap.
2. A truss in accordance with claim 1 wherein each of said first and second composite plate structures further comprises:
a second flange plate wherein said first flange plate and said second flange plate are oriented such that at least one of said plurality of web members is located therebetween.
3. A truss in accordance with claim 2 , wherein at least a portion of said second flange plate extends substantially perpendicular from said plurality of web members.
4. A truss in accordance with claim 1 wherein each of said first and second composite plate structures is formed from a plurality of sheets of a composite material, wherein said composited material is at least one of a plain weave composite material and a 5 hardness composite material.
5. A truss in accordance with claim 1 wherein said plurality of web members further comprise at least one of a vertical web member and a horizontal web member.
6. A truss in accordance with claim 1 , wherein said first composite plate structure and said second composite plate structure are oriented with respect to one another such that upon coupling, said truss comprises an aircraft wing truss rib assembly.
7. A truss in accordance with claim 1 , wherein the opening in each of said first and second plate composite structures is defined by vertical web members of said plurality of web members.