Lightweight composite single-skin sandwich lattice structures
A single-skinned composite lattice sandwich structure includes a face sheet, fiber stringers, and at least one fiber tow arranged in a lattice structure separating the face sheet and fiber stringers. The face sheet and at least the fiber tow(s) forming the lattice may be interfused with a matrix to form a contiguous composite structure. The fiber stringers may be formed of various materials for imparting different structural properties to the sandwich structure, including carbon fiber for tensile strength and lightness, metallic or other rigid material for imparting overall structural rigidity, shape-changing material or actuated material for providing actuated deformation of the structure, and may also include sensors.
1. A single-skinned composite lattice structure, comprising:
a face sheet formed of more than one layer of fiber fabric;
a plurality of stringers; and
a plurality of linear lattice members extending between the face sheet and the plurality of stringers and connecting with the face sheet and the plurality of stringers at a plurality of points, with at least one fiber tow extending through and forming a part of at least two of the plurality of lattice members; and a matrix material interfused with the at least one fiber tow and interfused into the face sheet to enhance weight savings by reducing sections of the composite lattice structure that are infused with the matrix material,
wherein the at least one fiber tow both abuts and weaves through the face sheet to form the single-skinned composite lattice structure,
the plurality of linear lattice members run in a pattern along a length of the single-skinned composite lattice structure forming pyramidal truss-like shapes,
and the plurality of stringers are connected with base ends of the pyramidal truss-like shapes formed by the plurality of linear lattice members, such that when the face sheet is loaded, the pyramidal truss-like shapes tend toward expansion putting the plurality of stringers in tension and thereby resulting in the single-skinned composite lattice structure being capable of consuming energy under high-load, impact, or blast conditions.
2. The single-skinned composite lattice structure of claim 1 , wherein:
at least a first fiber tow abuts an inferior surface of the face sheet.
3. The single-skinned composite lattice structure of claim 2 , wherein:
at least a second fiber tow is woven through a first portion of the face sheet from the inferior surface to a superior surface and returns through a second portion of the face sheet from the superior surface to the inferior surface.
4. The single-skinned composite lattice structure of claim 1 , wherein: at least a first fiber tow abuts a first portion of at least one of the plurality of stringers.
5. The single-skinned composite lattice structure of claim 4 , wherein: at least a second fiber tow winds about a second portion of the at least one of the plurality of stringers.
6. The single-skinned composite lattice structure of claim 5 , wherein the stringers comprise fibers, and wherein the matrix material is further infused throughout the plurality of fiber stringers.
7. The single-skinned composite lattice structure of claim 6 , wherein the fiber stringers comprise carbon fiber.
8. The single-skinned composite lattice structure of claim 1 , wherein:
each lattice member forming the pyramidal truss-like shapes has a face-sheet end and a stringer-end; and
each stringer-end of each lattice member is connected with at least two stringers at an intersection between the stringers.
9. The single-skinned composite lattice structure of claim 8 , wherein:
the plurality of stringers is arranged in a square cross-hatched pattern, such that intersecting pairs of stringers are orthogonal to each other; and
adjacent stringer-ends of adjacent lattice members are connected to adjacent intersections in the cross-hatched pattern.
10. The single-skinned composite lattice structure of claim 8 , wherein:
the plurality of stringers is arranged in a triangular crossing pattern, such that intersecting stringers are arranged at acute angles to each other; and
adjacent stringer-ends of adjacent lattice members are connected to adjacent intersections of stringers, such that the lattice forms a three-sided pyramidal truss pattern.
11. The single-skinned composite lattice structure of claim 1 , wherein the face sheet comprises a plurality of carbon fiber sheets arrayed in a stack; and the stack is arranged in a plurality of ply orientations.
12. A composite lattice structure, comprising:
a face sheet formed of more than one layer of fiber fabric;
a plurality of stringers; and
two or more lattice members extending between the face sheet and the plurality of stringers, wherein the two or more lattice members comprise:
at least two fiber tows; wherein
each fiber tow of the at least two fiber tows extends through and forms a part of a plurality of the lattice members and is in contact with the face sheet at a plurality of points on a surface of the face sheet and is in contact with at least one of the plurality of stringers, and wherein each fiber tow of the at least two fiber tows is substantially parallel and straight for a length of a first lattice member, curves proximate to the face sheet, then straightens again within a second lattice member; and
the at least two fiber tows and the face sheet are fixed in a contiguous matrix with a matrix material, wherein the at least two fiber tows are interfused with the matrix material and the matrix material is interfused into the face sheet to enhance weight savings by reducing sections of the composite lattice structure that are infused with the matrix material,
the two or more lattice members run in a pattern along a length of the composite lattice structure forming pyramidal truss-like shapes,
and the plurality of stringers are connected with base ends of the pyramidal truss-like shapes formed by the two or more lattice members, such that when the face sheet is loaded, the pyramidal truss-like shapes tend toward expansion putting the plurality of stringers in tension and thereby resulting in the composite lattice structure being capable of consuming energy under high-load, impact, or blast conditions.
13. The composite lattice structure of claim 12 , wherein the plurality of stringers is also fixed in the contiguous matrix with the interfused matrix material.
14. The composite lattice structure of claim 12 , wherein a first subset of the at least two fiber tows abuts an inferior surface of the face sheet; and a second subset of the at least two fiber tows is interwoven with at least a portion of the face sheet.
15. The composite lattice structure of claim 14 , wherein the face sheet further comprises a plurality of carbon fiber sheets arrayed in a stack; and wherein the second subset of the at least two fiber tows is interwoven with at least an inferior layer of the stack, and is not interwoven with at least a superior layer of the stack.
16. The composite lattice structure of claim 12 , wherein the plurality of stringers further comprises a strain sensor.
17. The composite lattice structure of claim 12 , wherein the plurality of stringers further comprises an actuator for changing a length of one or more of the plurality of stringers.
18. The composite lattice structure of claim 12 , wherein the plurality of stringers further comprises a shape memory material for changing a length of one or more of the plurality of stringers.