System and method for manufacturing a stiffened composite structure

Patent metadata

Field	Value
Publication number	US-10035300-B2
Application number	US-201514746844-A
Country	US
Kind code	B2
Filing date	Jun 23, 2015
Priority date	Jun 23, 2015
Publication date	Jul 31, 2018
Grant date	Jul 31, 2018

Abstract

A system for manufacturing a stiffened composite panel may include a stiffener tooling assembly, a caul plate, and a rotatable strongback. The stiffener tooling assembly may include stiffener tooling configured to support a plurality of composite stiffeners. The caul plate may have a layup surface for laying up a composite skin. The strongback may be releasably coupled to the caul plate. The system may include a plurality of hinges each having a fixed hinge portion and a movable hinge portion. The movable hinge portion may be coupled to the strongback for rotation thereof between an open position and a closed position for engagement of the caul plate with the stiffener tooling assembly.

First claim

What is claimed is:

1. A system for manufacturing a stiffened composite skin panel, comprising:
a stiffener tooling assembly including stiffener tooling configured to support a plurality of composite stiffeners;
a caul plate having a layup surface for laying up a composite skin;
a strongback releasably coupled to the caul plate;
a plurality of hinges each having a fixed hinge portion and a movable hinge portion, the movable hinge portion being coupled to the strongback for rotating between an open position and a closed position for engagement of the caul plate with the stiffener tooling assembly; and
a plurality of clamps configured to releasably clamp the strongback to the caul plate during rotation of the strongback and caul plate from the open position toward the closed position, the clamps configured to release the strongback from the caul plate when the caul plate is supported above the stiffener tooling assembly, thereby allowing the hinges to rotate the strongback back toward the open position without the caul plate.

2. The system of claim 1 , further including:
a counterbalancing system configured to counterbalance at least a portion of a mass of the strongback when the composite skin and the composite stiffeners are moved into contact with one another.

3. The system of claim 2 , wherein:
the counterbalancing system includes a plurality of linear actuators positioned along a strongback perimeter of the strongback; and
the linear actuators being configured to vertically move the strongback and the caul plate between a hover position and a docked position, the composite skin and composite stiffeners contacting one another in the docked position.

4. The system of claim 3 , wherein the counterbalancing system includes:
a plurality of posts positioned along a strongback perimeter of the strongback; and
one or more of the posts including a linear actuator.

5. The system of claim 3 , wherein:
the linear actuators are configured as hydraulic cylinders fluidly coupled to a hydraulic pressure controller configured to regulate hydraulic pressure at each hydraulic cylinder.

6. The system of claim 1 , further including:
one or more rotational actuators mounted to at least one of the hinges and configured to rotate the strongback.

7. The system of claim 1 , further comprising:
at least one indexing mechanism configured to index the strongback with the caul plate.

8. The system of claim 7 , wherein:
the indexing mechanism includes a ball fixture and a socket fixture mounted to the strongback and the caul plate.

9. The system of claim 1 , further comprising:
at least one alignment mechanism configured to align the caul plate to the stiffener tooling assembly, or vice versa.

10. A system for manufacturing a stiffened composite skin panel, comprising:
a stiffener tooling assembly including stiffener tooling configured to support a plurality of composite stiffeners;
a caul plate having a layup surface for supporting a composite skin;
a strongback;
a plurality of clamps configured to releasably clamp the strongback to the caul plate;
a plurality of hinges each having a linear actuator, a fixed hinge portion, and a movable hinge portion, the fixed hinge portion being coupled to a fixed object, the movable hinge portion being coupled to the strongback for rotation thereof between an open position and a closed position for engagement of the caul plate to the stiffener tooling assembly;
a plurality of linear actuators positioned on one or more sides side of the strongback when in the closed position;
the linear actuators cooperating to vertically lower the strongback and caul plate from a hover position to a docked position in which the composite skin is in contact with the composite stiffeners; and
the plurality of clamps are configured to clamp the strongback to the caul plate during rotation of the strongback and caul plate from the open position toward the closed position; and configured to release the strongback from the caul plate when the caul plate is supported by the linear actuators above the stiffener tooling assembly, thereby allowing the hinges to rotate the strongback back toward the open position without the caul plate.

11. A method for manufacturing a stiffened composite skin panel, comprising:
providing a caul plate including a layup surface supporting a composite skin;
providing a composite stiffener assembly including one or more composite stiffeners laid up on stiffener tooling;
releasably clamping, using a plurality of clamps, a strongback to the caul plate; and
rotating, using a plurality of hinges, the strongback coupled to the caul plate from an open position to a closed position for engagement of the composite skin with the composite stiffeners to form a stiffened composite skin panel, each one of the hinges having a fixed hinge portion and a movable hinge portion, the fixed hinge portion being coupled to a fixed object, the movable hinge portion being coupled to the strongback; and
the plurality of clamps are configured to clamp the strongback to the caul plate during rotation of the strongback and caul plate from the open position toward the closed position; and configured to release the strongback from the caul plate when the caul plate is supported by the linear actuators above the stiffener tooling assembly, thereby allowing the hinges to rotate the strongback back toward the open position without the caul plate.

12. The method of claim 11 , further including:
detaching the strongback from the caul plate and rotating the strongback toward the open position after engagement of the composite skin with the composite stiffeners.

13. The method of claim 11 , further including:
counterbalancing, using a counterbalancing system, at least a portion of a mass of the strongback when the composite skin and the composite stiffeners are moved into contact with one another.

14. The method of claim 13 , wherein the step of counterbalancing the strongback includes:
vertically lowering the strongback and the caul plate from a hover position to a docked position until the composite skin contacts the composite stiffeners.

15. The method of claim 14 , wherein the step of vertically lowering the strongback includes:
supporting and lowering the strongback using one or more linear actuators positioned along a perimeter of the strongback.

16. The method of claim 15 , wherein the linear actuators are hydraulic cylinders, the step of counterbalancing the mass of the strongback includes:
regulating, using a hydraulic pressure controller, hydraulic pressure in the hydraulic cylinders such that the hydraulic pressure at each hydraulic cylinder is apportioned according to a local mass fraction of the strongback.

17. The method of claim 11 , further including:
aligning, using at least one alignment mechanism, the caul plate with the stiffener tooling assembly when moving the composite skin and the composite stiffeners into contact with one another.

18. The method of claim 11 , wherein the step of rotating the strongback coupled to the caul plate includes:
rotating, using a first rotational actuator and a second rotational actuator of at least one of the hinges, the strongback coupled to the caul plate.

19. The method of claim 11 , further including:
indexing, using at least one indexing mechanism, the strongback with the caul plate.

20. The method of claim 19 , wherein the step of indexing the strongback with the caul plate includes:
engaging a ball fixture with a socket

Assignees

• Boeing Co

Inventors

• Encinosa Joe
• Barwick Andrew
• Bick Robert

Classifications

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C65/56

  using mechanical means {or mechanical connections, e.g. form-fits} · CPC title

• B29C33/26 Primary

  by pivotal movement · CPC title

• B29D99/0014

  provided with ridges or ribs, e.g. joined ribs · CPC title

• B29C65/48 Primary

  using adhesives {, i.e. using supplementary joining material; solvent bonding} · CPC title