Composite stiffener positioning and vacuum bag installation

Patent metadata

Field	Value
Publication number	US-9346221-B2
Application number	US-33945508-A
Country	US
Kind code	B2
Filing date	Dec 19, 2008
Priority date	Dec 19, 2008
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

A method and apparatus for manufacturing composite parts. An expandable tool with a transfer system may be moved on a surface of the expandable tool into an outer mold line tool with a composite material laid up on the outer mold line tool. The expandable tool may be expanded in the outer mold line tool to change the surface from a retracted state to an expanded state. The transfer system may be transferred from the expandable tool with the surface in the expanded state to the outer mold line tool.

First claim

What is claimed is:

1. A method for manufacturing composite parts, the method comprising:
moving an expandable tool with a vacuum bag system on a surface of the expandable tool into an outer mold line tool with a composite material laid up on the outer mold line tool;
expanding the expandable tool in the outer mold line tool to change the surface from a retracted state to an expanded state;
transferring the vacuum bag system from the expandable tool with the surface in the expanded state to the composite material laid up on the outer mold line tool;
retracting the expandable tool in the outer mold line tool to change the surface from the expanded state to the retracted state after transferring the vacuum bag system to the composite material;
removing the expandable tool from the outer mold line tool after transferring the vacuum bag system to the composite material; and
curing the composite material on the outer mold line tool after removing the expandable tool from the outer mold line tool.

2. The method of claim 1 , further comprising:
placing the vacuum bag system onto the surface of the expandable tool while the surface is in the retracted state.

3. The method of claim 1 , wherein the moving step comprises:
moving the expandable tool concentrically into the outer mold line tool.

4. The method of claim 1 , further comprising:
placing a number of composite elements on the expandable tool.

5. The method of claim 4 , wherein the transferring step comprises:
transferring the vacuum bag system and the number of composite elements from the expandable tool with the surface in the expanded state to the outer mold line tool.

6. The method of claim 5 , wherein the expanding step comprises:
expanding the expandable tool to change the surface from the retracted state to the expanded state to apply a force such that the vacuum bag system and the number of composite elements couple the composite material.

7. The method of claim 4 , wherein the moving step comprises:
moving the expandable tool with the vacuum bag system and the number of composite elements into the outer mold line tool with the composite material laid up on the outer mold line tool; and
aligning the number of composite elements on the expandable tool with a number locations for the number of composite elements.

8. The method of claim 4 , wherein the number of composite elements comprise at least one of a stringer, a composite ply, a screen, a metal ply, and a doubler.

9. The method of claim 1 , wherein the expandable tool comprises a support structure; a plurality of segments moveably connected to the support structure, wherein the plurality of segments form a surface system with the surface; and an actuator system capable of moving the plurality of segments to change a state of the surface between the retracted state and the expanded state.

10. The method of claim 9 , wherein the support structure comprises a reel; and a plurality of slide members connected to the reel, wherein each segment in the plurality of segments is slidably attached to a corresponding slide member in the plurality of slide members.

11. The method of claim 9 , wherein the actuator system comprises a plurality of linear actuators, wherein each segment in the plurality of segments is connected to an associated linear actuator in the plurality of linear actuators.

12. The method of claim 9 , wherein the reel has a channel and further comprises:
a shaft, wherein the reel is capable of receiving the shaft and wherein the shaft is capable of supporting the reel.

13. A method for installing components for a section of a composite aircraft fuselage, the method comprising:
placing a vacuum bag system onto a surface of an expandable tool while the expandable tool is in a retracted state;
placing a number of composite elements on the expandable tool after placing the vacuum bag system onto the surface, wherein the number of composite elements comprise at least one of a stringer and a doubler;
moving the expandable tool with the vacuum bag system and the number of composite elements into an outer mold line tool with a composite material laid up on the outer mold line tool;
aligning the number of composite elements on the expandable tool with a number locations for the number of composite elements;
expanding the expandable tool in the outer mold line tool to change the surface from a retracted state to an expanded state to apply a force such that the vacuum bag system and the number of composite elements adhere to the composite material;
transferring the vacuum bag system and the number of composite elements from the expandable tool with the surface in the expanded state to the outer mold line tool, wherein the vacuum bag system and the number of composite elements adhere to the composite material;
retracting the expandable tool in the outer mold line tool to change the surface from the expanded state to the retracted state after transferring the vacuum bag system and the number of composite elements to the outer mold line tool;
removing the expandable tool from the outer mold line tool after transferring the vacuum bag system and the number of composite elements to the outer mold line tool; and
curing the composite material on the outer mold line tool after removing the expandable tool from the outer mold line tool,
wherein the expandable tool comprises a support structure, a plurality of segments, and an actuator system, wherein the plurality of segments are moveably connected to the support structure and form a surface system with the surface, wherein the actuator system is capable of moving the plurality of segments to change a state of the surface between the retracted state and the expanded state, wherein the support structure comprises a reel and a plurality of slide members connected to the reel, wherein each segment in the plurality of segments is slidably attached to a corresponding slide member in the plurality of slide members; wherein the actuator system comprises a plurality of linear actuators, wherein each segment in the plurality of segments is connected to an associated linear actuator in the plurality of linear actuators, and wherein the reel has a channel that is capable of receiving a shaft, wherein the shaft is capable of support the reel.

Assignees

• Brennan Joseph D
• Darrow Donald Chester
• Dull Kenneth M
• Hollensteiner William S
• Noel Jennifer Sue
• Robins Brian G
• Jones Darrell D
• Boeing Co

Inventors

• Brennan Joseph D
• Darrow Donald Chester
• Dull Kenneth M
• Hollensteiner William S
• Noel Jennifer Sue
• Robins Brian G
• Jones Darrell D

Classifications

• B29C33/485

  cores or mandrels (collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824) · CPC title

• B29C70/30 Primary

  Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core · CPC title