Method and material efficient tooling for continuous compression molding

• US 10,414,107 B2
• Filed: 12/04/2017
• Issued: 09/17/2019
• Est. Priority Date: 02/03/2007
• Status: Active Grant

• Current Assignee: 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:
  US15/831,388
• Publication Number:
  US 20180154596A1
• Time in Patent Office: 652 Days
• 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 continuous compression molding fabrication line for performing a continuous process for forming a part using sheet members of composite material, the continuous compression molding fabrication line comprising:

a pre-forming zone configured to receive a plurality of sheet members of composite material, the pre-forming zone further configured to align and apply pressure to the sheet members to produce preformed sheet members;

a consolidation station configured to receive preformed sheet members from the preforming zone, the consolidation station comprising a heater that heats the preformed sheet members, followed by a plurality of tool dies individually mated with tool members having outer surfaces engaged by the plurality of tool dies and configured to compress heated preformed sheet members, followed by a cooling zone comprising a cooler configured to cool compressed heated preformed sheet members, and wherein the consolidation station has a first length through which the tooling is configured to pass during operation of the continuous compression molding fabrication line; and

tooling around which the sheet members are attached, the tooling initially connected to the pre-forming zone, the tooling configured to be drawn through the pre-forming zone and then through the consolidation station, the tooling further configured to reduce an amount of material required to manufacture the part, wherein the tooling is configured to reduce the amount of material required to manufacture by having;

a body having first and second ends,

the body including a recessed area,

the first and second ends of the body extending beyond the recessed area; and

a second length of a portion of the second end extending beyond the recessed area being greater than or equal to the first length of the consolidation station through which the tooling is configured to pass during operation of the continuous compression molding fabrication line.

2. The continuous compression molding fabrication line of claim 1, wherein the recess defines first and second shoulders in the body for respectively engaging an end of the part.

3. The continuous compression molding fabrication line of claim 1, wherein the recess has a depth substantially equal to a thickness of the part.

4. The continuous compression molding fabrication line of claim 1, wherein the recess has a depth such that outer surfaces of the tooling are substantially coplanar with outer surfaces of the part.

5. The continuous compression molding fabrication line of claim 1, wherein the body has a cross-sectional shape generally matching the cross-sectional shape of the part.

6. The continuous compression molding fabrication line of claim 1, wherein the body is elongate and the recess is formed in the body between the first and second ends of the body.

7. The continuous compression molding fabrication line of claim 1, wherein the first and second ends of the body have an outer surface extending substantially coplanar with an outer surface of the part.

8. The continuous compression molding fabrication line of claim 1, wherein the recessed area has the general shape of a part and the part is carried in the recessed area.

9. The continuous compression molding fabrication line of claim 1, wherein the recessed area has a depth that varies in at least one direction across the recessed area.

10. The continuous compression molding fabrication line of claim 1, wherein the body includes tooling features within the recessed area for forming shapes in the part.

11. The continuous compression molding fabrication line of claim 1, wherein a third length of a portion of the first end of the tooling extending beyond the recessed area is greater than or equal to a distance between a pulsating drive mechanism and the pre-forming zone, wherein the pulsating drive mechanism is positioned downstream from the consolidation station.

12. A continuous compression molding fabrication line for performing a continuous process for forming a part using sheet members of composite material, the continuous compression molding fabrication line comprising:

a pre-forming zone configured to receive a plurality of sheet members of composite material, the pre-forming zone further configured to align and apply pressure to the sheet members to produce preformed sheet members;

a consolidation station configured to receive preformed sheet members from the preforming zone, the consolidation station comprising a heater that heats the preformed sheet members, followed by a plurality of tool dies individually mated with tool members having outer surfaces engaged by the plurality of tool dies and configured to compress heated preformed sheet members, followed by a cooling zone comprising a cooler configured to cool compressed heated preformed sheet members, and wherein the consolidation station has a first length through which the tooling is configured to pass during operation of the continuous compression molding fabrication line; and

tooling around which the sheet members are attached, the tooling initially connected to the pre-forming zone, the tooling configured to be drawn through the pre-forming zone and then through the consolidation station, the tooling further configured to reduce an amount of material required to manufacture the part, wherein the tooling is configured to reduce the amount of material required to manufacture by having;

a body having opposite first and second ends, the body being elongate,

the bony having at least one recess,

the first and second ends of the body extending respectively beyond opposite ends of the at least one recess and having outside surfaces forming an extension of a profile of the part when the plurality of sheet members is compressed into a shape of the part, and wherein a second length of a portion of the second end extending beyond the recessed area is greater than or equal to the first length of the consolidation station through which the tooling is configured to pass during operation of the continuous compression molding fabrication line.

13. The continuous compression molding fabrication line of claim 12, wherein the at least one recess has the general shape of the part and the plurality of sheet members are received within the at least one recess.

14. The continuous compression molding fabrication line of claim 12, wherein the at least one recess has a depth substantially equal to a thickness of the part.

15. The continuous compression molding fabrication line of claim 12, wherein the outside surfaces of the body are substantially coplanar with exterior surfaces of the part.

16. The continuous compression molding fabrication line of claim 12, wherein the at least one recess defines first and second shoulders in the body, and the first and second shoulders engage opposite ends of the part.

17. The continuous compression molding fabrication line of claim 12, wherein body has a cross-sectional shape generally matching the cross-sectional shape of the part.

18. The continuous compression molding fabrication line of claim 12, wherein a portion of the first end of the body extends beyond the at least one recess a distance sufficient such that at least portions of the first end of the body pass through the continuous compression molding fabrication line before the plurality of sheet members enters the continuous compression molding fabrication line.

19. The continuous compression molding fabrication line of claim 12, wherein a portion of the second end of the body extends beyond the at least one recess a distance sufficient such that at least portions of the second end of the body remain in the continuous compression molding fabrication line after the plurality of sheet members has passed through the molding line.

20. The continuous compression molding fabrication line of claim 12, wherein the at least one recess has a non-uniform depth.

21. The continuous compression molding fabrication line of claim 12, wherein the body includes tooling features within the at least one recess for forming shapes in the part.

22. The continuous compression molding fabrication line of claim 12, wherein a third length of a portion of the first end of the tooling is greater than or equal to a distance between a pulsating drive mechanism and the pre-forming zone, wherein the pulsating drive mechanism is positioned downstream from the consolidation station.

23. The continuous compression molding fabrication line of claim 12, wherein the body is rigid.

24. A continuous compression molding fabrication line for performing a continuous process for forming a part using sheet members of composite material, the continuous compression molding fabrication line comprising:

a pre-forming zone configured to receive a plurality of sheet members of composite material, the pre-forming zone further configured to align and apply pressure to the sheet members to produce preformed sheet members;

a consolidation station configured to receive preformed sheet members from the preforming zone, the consolidation station comprising a heater that heats the preformed sheet members, followed by a plurality of tool dies individually mated with tool members having outer surfaces engaged by the plurality of tool dies and configured to compress heated preformed sheet members, followed by a cooling zone comprising a cooler configured to cool compressed heated preformed sheet members, and wherein the consolidation station has a first length through which the tooling is configured to pass during operation of the continuous compression molding fabrication line; and

tooling around which the sheet members are attached, the tooling initially connected to the pre-forming zone, the tooling configured to be drawn through the pre-forming zone and then through the consolidation station, the tooling further configured to reduce an amount of material required to manufacture the part, wherein the tooling is configured to reduce the amount of material required to manufacture by having;

an elongate body having a leading end, a central section, and a trailing end, in which a portion of a second length of the leading end of the tool is greater than or equal to the first length; and

at least one recess positioned within the central section.