System for additive manufacturing

1. A method of manufacturing a composite structure, comprising:

directing a reinforcement tape that is pre-impregnated with a matrix past a heat source to tackify the reinforcement tape;

compacting the tacky reinforcement tape to form a first portion of the composite structure;

wetting a reinforcement with a matrix in-situ;

placing the wetted reinforcement in a repeated geometric pattern to build up layers of substantially identical prisms that are adjacent to and connected to each other at an intersection, wherein the intersection includes multiple crossing points that deviate from the repeated geometric pattern and alternate locations between overlapping layers;

compacting the wetted reinforcement to form a second portion of the composite structure;

at least triggering curing the matrix; and

autoclaving the composite structure to complete curing of the tacky reinforcement tape and the matrix.

2. The method of claim 1 , wherein:

the first portion of the composite structure is at least one of a shell and a skin; and

the second portion of the composite structure is a core.

3. The method of claim 1 , wherein the locations are oriented about 90° from each other relative to a center point of the intersection.

4. The method of claim 1 , wherein the multiple crossing points are oriented about 180° from each other within the same layer relative to a center point of the intersection.

5. A method of manufacturing a composite structure, comprising:

directing a reinforcement tape that is pre-impregnated with a matrix past a heat source to tackify the reinforcement tape;

compacting the tacky reinforcement tape to form a first portion of the composite structure;

wetting a reinforcement with a matrix in-situ;

compacting the wetted reinforcement to form a second portion of the composite structure;

at least triggering curing the matrix; and

autoclaving the composite structure to complete curing of the tacky reinforcement tape and the matrix, wherein the reinforcement includes at least one of a metallic wire and an optical tube, and the method further includes selectively activating the at least one of the metallic wire and the optical tube after application to expose the first portion to energy that facilitates curing of the reinforcement tape.

6. A method of manufacturing a composite structure, comprising:

depositing a pre-impregnated reinforcement tape, including at least one of a metallic wire and an optical tube, against a surface to form a first portion of the composite structure;

wetting a reinforcement with a matrix in-situ;

depositing the wetted reinforcement to form a second portion of the composite structure;

at least partially curing the matrix to retain a shape of the second portion; and

heating the composite structure to complete curing of at least the pre-impregnated reinforcement tape,

wherein at least partially curing the matrix results in an exothermic reaction that at least partially cures the pre-impregnated reinforcement tape.

7. The method of claim 6 , wherein heating the composite structure also completes curing of the matrix.

8. The method of claim 6 , wherein at least partially curing the matrix includes exposing the matrix to a cure energy.

9. The method of claim 8 , wherein the cure energy is light.

10. The method of claim 6 , wherein the surface is formed by the wetted reinforcement.

11. The method of claim 6 , wherein depositing the wetted reinforcement includes depositing the wetted reinforcement against the deposited pre-impregnated reinforcement tape.

12. The method of claim 6 , further including tackifying the pre- impregnated reinforcement tape prior to depositing the pre-impregnated reinforcement tape.

13. The method of claim 6 , wherein:

the pre-impregnated reinforcement tape includes a tape pre-impregnated with a thermoset resin; and

the matrix is a thermoset resin.