Claims
- 1. A diaphragm chamber molding apparatus comprising:
a chamber for containing a mold surface therein; a bottom flexible diaphragm placed over and sealable with respect to the top of said chamber; a top flexible diaphragm placed over and sealable with respect to said bottom diaphragm for containing a lay-up between said top and bottom diaphragms; means for evacuating the area between said top and bottom diaphragms; and means for drawing said top and bottom diaphragms and said lay-up therebetween over a mold surface located in said chamber to form said lay-up.
- 2. The diaphragm chamber molding apparatus of claim 1 further including a source for applying heat to said diaphragms and said lay-up therebetween.
- 3. The diaphragm chamber molding apparatus of claim 1 in which said chamber includes a seal around the top thereof for engaging said bottom diaphragm and sealing said bottom diaphragm with respect to the top of said chamber.
- 4. The diaphragm chamber molding apparatus of claim 1 in which said top and bottom diaphragms are secured in top and bottom frames.
- 5. The chamber diaphragm molding apparatus of claim 4 in which said top frame includes a pressure seal for sealing said top frame with respect to said bottom diaphragm.
- 6. The diaphragm chamber molding apparatus of claim 1 in which said means for evacuating the area between said top and bottom diaphragms includes a vacuum pump connected to evacuate air from between said top and bottom diaphragms.
- 7. The diaphragm chamber molding apparatus of claim 1 in which said means for drawing said top and bottom diaphragms over a mold surface located in said chamber includes a vacuum pump connected to said chamber for evacuating air from within said chamber sealed by said bottom diaphragm to draw said top and bottom diaphragms down over said mold surface.
- 8. The diaphragm chamber molding apparatus of claim 1 further including control and monitoring apparatus for operating said means for evacuating the air between said top and bottom diaphragms and for operating said means for drawing said top and bottom diaphragms and a lay-up therebetween down over a mold surface located in said chamber and for monitoring the status of said means for evacuating and said means for drawing.
- 9. A method of forming a composite part, the method comprising:
assembling a lay-up on a template; forming said lay-up in a diaphragm chamber molding apparatus including top and bottom diaphragms elastically deformable over a mold surface, said lay-up placed between said diaphragms, said diaphragms and said lay-up therebetween stretched over the mold surface for forming said lay-up to correspond to the contours of said mold surface; in which assembling said lay-up includes providing tails extending beyond said template so that the top diaphragm grips said tails for stretching said lay-up and reducing wrinkles in said lay-up during forming.
- 10. The method of claim 9 in which said lay-up comprises a plurality of layers of a fiber reinforced thermoset resin material.
- 11. The method of claim 9 in which assembling said lay-up includes placing a plurality of layers of a fiber reinforced thermoset resin material on a template such that said tails increase in length in the layers proximate the template.
- 12. The method of claim 10 in which said tails are formed by extending said fiber reinforced thermoset resin material beyond said template.
- 13. The method of claim 10 in which said tails are formed from a material other than said fiber reinforced thermoset resin material.
- 14. The method of claim 9 further including the step of monitoring and controlling the temperature and viscosity of said lay-up dynamically during forming.
- 15. The method of claim 9 further including the step of evacuating air from between said top and bottom diaphragms.
- 16. The method of claim 9 further including the step of evacuating air from within said chamber molding apparatus.
- 17. The method of claim 9 further including the step of configuring said mold surface and/or said chamber to accentuate the stretching of said diaphragms.
- 18. The method of claim 17 in which the step of configuring includes placing forming members proximate said mold surface for increasing the stretching of said diaphragms and consequently said tails.
- 19. The method of claim 17 in which the step of configuring includes placing forming members between said diaphragms to accentuate the stretching of said diaphragms.
- 20. The method of claim 9 further including the step of evaluating the viscosity characteristics of the material used in said lay-up prior to forming to facilitate forming during optimal conditions.
- 21. The method of claim 20 in which forming includes the step of achieving the minimum viscosity of the material before said lay-up is stretched over said mold surface.
- 22. The method of claim 9 further including the step of rolling said lay-up to reduce wrinkles in said lay-up during forming.
- 23. The method of claim 9 further including the step of preparing said lay-up for removal from said mold surface after forming.
- 24. The method of claim 23 in which said step of preparing includes supercooling said lay-up.
- 25. The method of claim 23 in which said step of preparing includes curing said lay-up.
- 26. The method of claim 24 wherein supercooling includes packing said lay-up in dry ice while it is still in said diaphragm chamber molding apparatus.
- 27. The method of claim 9 further including the step of trimming said tails from said lay-up after it is formed.
- 28. The method of claim 9 further including the step of placing said lay-up in an autoclave after it is removed from the mold surface.
- 29. A method of forming a composite part, the method comprising:
assembling a lay-up on a template; forming said lay-up between top and bottom diaphragms elastically deformable over a mold surface, said lay-up placed between said diaphragms, said diaphragms and said lay-up therebetween stretched over said mold surface for forming said lay-up to correspond to the contours of said mold surface; in which assembling the lay-up includes providing tails extending beyond said template so that the top diaphragm grips said tails for stretching the lay-up and reducing wrinkles in said lay-up during forming; and evaluating the viscosity characteristics of the material used in said lay-up to facilitate forming during optimal conditions.
RELATED CASES
[0001] This application is a Continuation-In-Part of U.S. Ser. No. 08/271,561, filed Jul. 7, 1994, entitled “RESIN TRANSFER MOLDING SYSTEM AND METHOD” by Bernardon et al., which is a Continuation-In-Part of U.S. Ser. No. 07/869,384, filed Apr. 15, 1992, entitled “RESIN TRANSFER MOLDING SYSTEM AND METHOD” by Bernardon et al., which is a Continuation-In-Part of U.S. Ser. No. 07/675, 819 filed Mar. 27, 1991, entitled “RECONFIGURABLE FIBER-FORMING RESIN TRANSFER SYSTEM” by Bernardon et al.
Divisions (1)
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Number |
Date |
Country |
Parent |
08487858 |
Jun 1995 |
US |
Child |
08683928 |
Jul 1996 |
US |
Continuation in Parts (3)
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Number |
Date |
Country |
Parent |
08271561 |
Jul 1994 |
US |
Child |
08487858 |
Jun 1995 |
US |
Parent |
07869384 |
Apr 1992 |
US |
Child |
08271561 |
Jul 1994 |
US |
Parent |
07675819 |
Mar 1991 |
US |
Child |
07869384 |
Apr 1992 |
US |