Method and material efficient tooling for continuous compression molding

• US 8,491,745 B2
• Filed: 02/03/2007
• Issued: 07/23/2013
• Est. Priority Date: 02/03/2007
• Status: Active Grant

• Current Assignee: M/C 1640-2101, The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Wilkerson, Randall D., Fox, James R., Rubin, Alexander M.
• Primary Examiner(s): BELL, WILLIAM P
• Application Number:
  US11/701,789
• Publication Number:
  US 20080185756A1
• Time in Patent Office: 2,362 Days
• Field of Search: 264/297.4, 264/297.5, 264/297.6, 264/323, 265/297.7, 156/307.1, 156/245, 156/200, 156/201, 156/202, 156/553, 156/580, 414/222.05, 414/222.06, 425/323, 425/347, 425/353, 425/354, 425/355, 425/357, 425/359, 425/397, 425/400
• US Class Current: 156/245
• CPC Class Codes: B29C 43/14 in several steps
• CPC Class Codes: B29C 43/22 of articles of indefinite length
• CPC Class Codes: B29C 43/228 using endless belts feeding the material between non-rotating pressure members, e.g. vibrating pressure members
• CPC Class Codes: B29C 70/42 for producing articles of definite length, i.e. discrete articles
• CPC Class Codes: B29C 70/526 Pultrusion dies, e.g. dies with moving or rotating parts B29C70/523 takes precedence
• CPC Class Codes: B29C 70/54 Component parts, details or accessories; Auxiliary operations , e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
• CPC Class Codes: B29D 7/01 Films or sheets
• CPC Class Codes: B29K 2105/08 of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
• CPC Class Codes: Y10T 156/101 Prior to or during assembly with additional lamina
• CPC Class Codes: Y10T 156/1737 Discontinuous, spaced area, and/or patterned pressing

Abstract

Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.

Claims

1. A method of fabricating a thermoplastic laminate part comprising multiple laminate plies using a continuous compression molding line, comprising the steps of;

placing a lay-up comprising multiple laminate plies in a recess within a tool, the tool comprising a leading end, a central section, and a trailing end, the recess positioned within the central section of the tool; and

,

moving the tool through a continuous compression molding line to form the thermoplastic laminate part, the leading end of the tool entering a pulsating drive mechanism before the lay-up enters a pre-forming zone of the continuous compression molding line.

2. The method of claim 1, wherein moving the tool through the continuous compression molding line comprises pulling the tool through the continuous compression molding line by the pulsating drive mechanism.

3. The method of claim 2, wherein pulling the tool through the continuous compression molding line comprises:

grasping the leading end of the tool, and

pulling the leading end of the tool.

4. The method of claim 1, further comprising the steps of:

shaping the lay-up into a preformed part as the lay-up passes through the pre-forming zone;

consolidating the preformed part into a consolidated part as the preformed part passes through a consolidation operation;

cooling the consolidated part to form the thermoplastic laminate part; and

,

removing the thermoplastic laminate part from the tool.

5. The method of claim 1, wherein moving the tool comprises using a trailing end of the tool configured to maintain a substantially constant gap between press elements while the lay-up moves through the press elements of the continuous compression molding line.

6. The method of claim 1, wherein longitudinal movement of the lay-up relative to the tool is prevented by using shoulders on the tool within the recess to respectively abut opposite ends of the lay-up.

7. The method of claim 1, wherein a length of the leading end of the tool is greater than or equal to a distance between the pulsating drive mechanism and the pre-forming zone of the continuous compression molding line.

8. The method of claim 1, wherein a length of the trailing end of the tool is greater than or equal to a length of a consolidation station of the continuous compression molding line.

9. A method of fabricating a composite material part comprising multiple laminate plies using a continuous compression molding line, comprising the steps of:

supporting a lay-up of composite material comprising multiple laminate plies in a recess within a tool, a top of the lay-up within the tool exposed, the top of the lay-up and a length of the recess corresponding respectively to a top and total length of the composite material part, the recess defining a pair of oppositely facing shoulders within a thickness of a central section of the tool;

moving the tool through the continuous compression molding line including moving a portion of the tool through the continuous compression molding line and into a pulsating drive mechanism before the lay-up enters the continuous compression molding line;

shaping the lay-up into a preformed part as the tool moves through a pre-forming zone of the continuous compression molding line;

consolidating the preformed part as the tool moves through a consolidation station of the continuous compression molding line to form the composite material part such that a depth of the recess is substantially equal to a wall thickness of the composite material part; and

,

removing the composite material part from the tool.

10. The method of claim 9, further comprising:

preventing longitudinal movement of the lay-up relative to the tool by using the shoulders on the tool within the recess to respectively abut opposite ends of the lay-up.

11. The method of claim 9, wherein moving the tool comprises:

grasping a leading end of the tool, and

pulling the leading end of the tool.

12. The method of claim 11, wherein a length of the leading end of the tool is greater than or equal to a distance between the pulsating drive mechanism and the pre-forming zone of the continuous compression molding line.

13. The method of claim 9, further comprising:

maintaining a substantially constant gap between press elements in the continuous compression molding line at least until the recess exits the continuous compression molding line.

14. The method of claim 13, wherein maintaining the substantially constant gap comprises a trailing end of the tool within the continuous compression molding line until the composite material part has passed through the continuous compression molding line.

15. The method of claim 14, wherein a length of the trailing end of the tool is greater than or equal to a length of the consolidation station of the continuous compression molding line.

16. The method of claim 9, wherein moving the tool through the continuous compression molding line comprises moving the tool incrementally using a pulsating drive.

17. A method of fabricating a thermoplastic laminate part comprising multiple laminate plies using a continuous compression molding line, comprising the steps of:

placing a composite lay-up comprising multiple laminate plies in a recess within a tool;

moving the tool through a consolidation station in the continuous compression molding line by pulling a leading end of the tool through the continuous compression molding line;

consolidating the composite lay-up into the thermoplastic laminate part at the consolidation station as the tool is pulled through the continuous compression molding line to form the thermoplastic laminate part such that a depth of the recess is substantially equal to a wall thickness of the thermoplastic laminate part; and

,

using a trailing end of the tool to maintain an alignment within the consolidation station until the lay-up has been consolidated into the thermoplastic laminate part, a length of the trailing end of the tool being greater than or equal to a length of the consolidation station of the continuous compression molding line.

18. The method of claim 17, wherein pulling the leading end of the tool is performed incrementally using a pulsating drive.

19. The method of claim 17, wherein consolidating the composite lay-up is commenced only after the leading end of the tool has passed through the consolidation station and into a pulsating drive mechanism.

20. The method of claim 17, further comprising:

preventing longitudinal movement of the lay-up relative to the tool by using shoulders on the tool within the recess to respectively abut opposite ends of the lay-up.

21. The method of claim 17, wherein the trailing end of the tool remains in the consolidation station until the lay-up has been consolidated into the thermoplastic laminate part.

22. The method of claim 17, wherein a length of the leading end of the tool is greater than or equal to a distance between a pulsating drive mechanism pulling the leading end of the tool through the continuous compression molding line and the consolidation station of the continuous compression molding line.