System and method for promoting inter-ply slippage
A composite part forming system for shaping a composite material blank having a plurality of plies, the composite part forming system comprising opposing tools including shape-forming features, an actuator, and a composite tensioning system. The composite tensioning system is connectable to a periphery of the composite material blank to apply tension to the composite material blank the first and second tools are moved together to cause the composite material blank to conform to the shape-forming features. The composite tensioning system is configured to apply more tension to wrinkle prone plies of the composite material blank than to non-wrinkle prone plies as the composite material blank is caused to conform to the shape-forming features.
1. A method of shaping a composite material blank comprising plies, the method comprising steps of:
positioning a plurality of clevises near tension openings in the composite material blank;
extending a plurality of clevis pins through the tension openings;
connecting the plurality of clevis pins to the plurality of clevises so that the plurality of clevises are connected to the composite material blank;
applying tension to the composite material blank via the plurality of clevises and plurality of clevis pins such that more tension is applied to wrinkle prone plies of the composite material blank than to non-wrinkle prone plies of the composite material blank as the composite material blank is caused to conform to shape-forming features of a first tool; and
shaping the composite material blank to have a bend while applying tension, wherein the wrinkle prone plies define a concave surface at the bend and the non-wrinkle prone plies define a convex surface at the bend.
2. The method of claim 1 , further comprising a step of orienting the plurality of clevis pins diagonally relative to the plurality of clevises and the composite material blank.
3. The method of claim 1 , wherein the plurality of clevis pins include step-down ledges.
4. The method of claim 1 , wherein the plurality of clevis pins are cantilever pins and the step of extending the plurality of clevis pins through the tension openings includes extending the plurality of clevis pins only partially through the tension openings.
5. The method of claim 1 , wherein the step of connecting the plurality of clevis pins to the plurality of clevises includes extending the plurality of clevis pins through clevis pin holes of the plurality of clevises.
6. The method of claim 1 , wherein the step of applying tension is performed via a biasing element.
7. The method of claim 6 , further comprising a step of connecting the biasing element to the plurality of clevises via a plurality of tension wires.
8. The method of claim 1 , further comprising a step of moving a portion of the composite tensioning system to control the tension.
9. The method of claim 1 , further comprising a step of actuating a second tool toward the first tool to conform the composite material blank to the shape-forming features of the first tool.
10. The method of claim 1 , further comprising a step of inflating an inflatable bladder against the composite material blank to conform the composite material blank to the shape-forming features of the first tool.
11. The method of claim 1 , further comprising a step of suspending the composite material blank over the first tool.
12. A method of shaping a composite material blank comprising plies and tension openings, the method comprising steps of:
extending a plurality of cantilever pins through the tension openings; and
applying tension to the composite material blank via the plurality of cantilever pins such that more tension is applied to wrinkle prone plies of the composite material blank than to non-wrinkle prone plies of the composite material blank as the composite material blank is caused to conform to shape-forming features of a first tool; and
shaping the composite material blank to have a bend while applying tension, wherein the wrinkle prone plies define a concave surface at the bend and the non-wrinkle prone plies define a convex surface at the bend.
13. The method of claim 12 , wherein said extending the plurality of cantilever pins through the tension openings comprises extending each cantilever pin through an entire thickness of the composite material blank.
14. The method of claim 12 , wherein each cantilever pin includes a neck, a head, and a distal end opposite the head.
15. The method of claim 14 , further comprising attaching wires to the distal ends of the cantilever pins.
16. The method of claim 15 , wherein said extending the plurality of cantilever pins through the tension openings comprises engaging the head of each cantilever pin with the composite material blank to anchor the cantilever pin in the respective tension opening.
17. The method of claim 15 , wherein said applying tension comprises tensioning the wires to pull the cantilever pins via the distal ends.
18. The method of claim 17 , wherein said extending the plurality of cantilever pins through the tension openings comprises locating the distal ends of the cantilever pins adjacent the wrinkle prone plies and the head of the cantilever pins adjacent the non-wrinkle prone plies.